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PHOTOPOLARIMETRIC STUDIES OF COMETS

AND

OTHER OBJ ECTS

A Thesis SubmittedTo

Assam University, Silchar

For the Degree of Doctor of Philosophy

By

HIMADRI SEKHAR DAS

Registration Number: Ph. D./119/2002

Under the guidance of

Dr. ASOKE KUMAR SEN

DEPARTMENT OF PHYSICS, SCHOOL OF PHYSICAL SCIENCESASSAM UNIVERSITY, SILCHAR

Assam, India – 788011

November - 2004

© Himadri Sekhar Das



Dedicated to .............

Bappu and Mamani



Declaration

I hereby declare that this thesis submitted to Assam University, Silchar, for the

award of a Ph. D. degree, is a result of the investigations carried out by me under

the supervision of Dr. Asoke Kumar Sen. The results presented herein have not

been subjected to scrutiny, by any university or institute, for the award of a degree,diploma, associateship or fellowship whatsoever.

Dr. Asoke Kumar Sen Himadri Sekhar Das

(Thesis Supervisor) (Ph. D. Candidate)

Department of Physics

Assam University

Silchar-788011, India



29 November , 2004

Certificate

This is to cerify that Sri Himadri Sekhar Das , s/o Sri Himangshu Sekhar Das,

and Smt. Purabi Das, has been working with me since March, 2000 under my

guidance for Ph. D. His work entitled “Photopolarimetric studies of comets and

other objects” is bona fide, original and outcome of elaborate mathematical

analysis with physical interpretation. During the entire period of research work,

he has been consulting me at every stage and has completed all the formalities

as Ph. D. scholar. It is further certified that the work presented in this thesis has

not been submitted before for a degree or diploma to this university or any other

university or institutes of learning.

Dr. Asoke Kumar Sen



Acknowledgements

Whenever there is a question let it live. This, as a doctrine, has been a guiding force

for me since long. It was this force that initiated me to have undertaken a researchwork which, after years of painstaking labour, has now culminated in the shape of

this thesis. We all know, in this universe there are more and more questions beyond

the limit of all answers. There are waves of light , as well, to break into wisdom’s

widening shore. I have dared to tread in the ever-expanding domain of knowledge

only to carry forward the legacy of the eternal quest of mankind. On the outset,

the complexity of the subject I undertook as my research topic did appal me, but

as the time progressed the nature of my ndings overwhelmed me thoroughly. The outcome is here to be judged by you all.

I’m extremely grateful to Dr. Asoke Kumar Sen who with his vast erudition and

patient mind as a Research-Guide sailed me through all obstacles - academic as well

as administrative - to accomplish the project successfully. All along, the help I got

from him and the discussion with him were motivations to do better each time. I

thank him for the lessons learnt in the process which will help me to go forward.

I express my sincere gratitude to Prof. Subhash Chandra Saha, Vice Chancellor,

Assam University, who supported my endeavour whole heartedly.

I am also thankful to Prof. M. R. Islam, Dean, School of Physical Sciences for his

kind co-operation.

Thanks are due to a number of faculties in the Department without whose inter-

vention and moral support this work would not have been accomplished. I express

my gratitude to Dr. Ramendu Bhattacharjee, Reader and former Head, who al-

ways inspired me in this research work. His valuable suggestions and tips helped

me to complete the journey of one innings. I am thankful to Mr. A. C. Borah who

helped me in every steps. I am also grateful to Dr. P. Chakraborty for providing me

LATEX style le for this thesis writing. Whenever I had any problem, he immedi-

ately responded and try to solve the problem. I thank Dr. I. Sharma for his moral

support. I , further express, my gratitude to all my teachers in Assam University.

The non-teaching staff members of the Physics Department also deserve special men-

tion for their generous co-operation. I profusely thank Mr. Subrata Bhattacharjee,



Mr. Joydeep Choudhury, Mr. Sibasish Bhattacharjee, Mr. Monotosh Das, Mr. San-

joy Paul, Mr. Nilu Kanta Das and Mr. G. M. Laskar. I also express my gratitude

to other non-teaching members of Assam University.

Research scholars who were genius enough in extending their helping hands whenever

required. I thank Smt. Indira Dey, Smt. Parvin Sultana Laskar, Raghu Nandan Das,

Rahul Bhattacharjee, Manoj Kumar Paul, Sudip Choudhury, Sanjib Sheel and other

research scholars. I take this opportunity to appreciate and express my gratitude to

my friends: Manas , Paplu, Nripacharya, Joydeep, Dipak and others.

I thank Mr. Abhijit Deb, Headmaster, Irongmara High School, who always inspired

me like my elder brother. I profusely thank Mr. Parimal Shuklabaidya and Mrs.

Uma Shuklabaidya for their kind cooperation.

I also thank Dr. R. R. Chakraborty, Principal, Karimganj College and Mr. A. K.

Das, Head, Dept. of Physics in the same college for their moral support.

I also thank my family members that comprise of my parents Shri Himangshu Sekhar

Das and Smt. Purabi Das; my elder sisters Paramita and Jayita; my brothers in

law Amit and Sougata; my nephew Akash and Megh, who were ever response to my

mental needs thus being my sources of inspiration in the days when I needed it most.

I’m highly grateful to Dr. Subir Kar, Reader, Dept. of Bengali, Assam University,

who as a family member always guided me. His mental support encouraged me

during the period of research.

I’m also grateful to the authority and other members at IUCAA, Pune for making

their library and the Computer Center available to me whenever I have been to their

campus.

I’m grateful to Dept. of atomic Energy (DAE), Govt. of India for the project

(BRNS/98/37/6)under which this research work has been done and I was awarded

the fellowship. It would not have been possible for me to continue this work without

the nancial assistance from DAE. I also express my gratitude to Dr. C. L. Kaul

( Ex Director NRL/HARL, BARC, Mumbai) and Principal Collaborator(PC) of

this project, for useful technical and scientic discussions, without which this thesis

would have been incomplete.



AbstractCometary polarimetry in the continuum is a good technique to investigate the nature

of dust grains. Several investigators studied linear and circular polarisations of

different comets, which are caused mainly due to scattering of sunlight by cometary

dust. The scattering properties of a particle depend upon: ( i) the complex refractive

index of the particle, m = n −ik, where n and k are the refractive and absorptive

indices respectively, ( ii ) the wavelength of the incident solar radiation ( λ), (iii ) the

size of the particle (a) and ( iv) scattering angle ( θ).

The theory of scattering of light by small particles is basic to the study of cometary

grains. Actually, this theory determines the distribution of intensity of the scat-

tered radiation and the polarisation as a function of the scattering angle. Several

scattering theories have been developed for well-dened particle shapes like spheres,

concentric spheres, cylinders, spheroids and so on. Among them Mie Theory, T-

matrix theory, Discrete Dipole Approximation etc. are widely used. Mie theory

provides an analytic solution to the general scattering problem for spheres and cor-

rectly describes the interaction of light with dust grains that are small compared

to the wavelength of light. But cometary grains may contain irregular shape par-

ticles. Recently, T-matrix theory has been used by many investigators to interpret

the polarisation data of comets.

In this work, several comets (viz., comets Halley, Hale-Bopp, Hyakutake, Austin,

Levy 1990XX, Bradeld etc) are studied using Mie theory. Also comet Levy 1990XX

is studied using T-matrix theory. Besides polarisations observed for some star form-

ing clouds are also studied.

Different chapters are organised as below:

The Chapter 1 deals with a historical account of the development of cometary

science. The basic denition of comets, its structure, classication and origin are

discussed. A brief description of the nature of cometary dust is also given. The

comets and their important role in Solar System studies are then discussed. Finally

the objective and the layout of the thesis are presented.

In Chapter 2 , Photometric, Spectrometric and Polarimetric (Optical) measurements

on comets are discussed. Observations at other wavelengths (e.g., Infra red, Ultra



Violet, X-ray and Radio) are then discussed. Finally in situ observations of comets

are presented.

In Chapter 3 , the basic denitions of polarisation in terms of Stokes parameters are

discussed. Then the properties of Stokes parameters, transformation matrix and

transformation equation for Stokes parameters are discussed. Different errors in po-

larisation measurements are then discussed. Finally, different kinds of polarimeters

are discussed.

The Chapter 4 begins with the introduction of different light scattering theories

which are used for the study of cometary grains. Then Mie scattering theory for

spherical particles is discussed. The in situ dust measurements of comet Halley are

also discussed. Finally, the polarimetric data of comet Halley is analysed using Mie

Theory.

In Chapter 5 , polarimetric observations on several comets are discussed. Then ob-

served variation in polarisation properties between different comets is discussed.

Also a model is proposed to explain this observed variation, in terms of grain aging

of comets by solar radiation.

In Chapter 6 , T-matrix theory is discussed. Then the polarimetric data of comet

Levy 1990XX is analysed using Mie and T-matrix theory. Finally, the negative

polarisation behaviour of comet Levy 1990XX is discussed.

In Chapter 7 , discussions are made on the polarisations which have been observed

for stars background to several star forming clouds. The observed polarisations are

interpreted in terms of the on going star forming processes in the cloud.





3. H. S. Das , A. K. Sen, 2004. Polarimetric studies of comet Levy 1990XX. An

oral presentation at the fourth conference on Physics Research in North East,

(November 5-6, 2004), hosted by Gurucharan College, Silchar



Contents

List of Figures xii

List of Tables xiv

1 INTRODUCTION 1

1.1 A brief historical account of Cometary science: . . . . . . . . . . . . . . 1

1.2 Structure of comets: . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

1.3 Classication of comets: . . . . . . . . . . . . . . . . . . . . . . . . . 3

1.4 Origin of comets: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

1.5 The nature of Cometary Dust: . . . . . . . . . . . . . . . . . . . . . . 6

1.6 The comets and its important role in Solar System studies . . . . . . 10

1.7 The Objective and Layout of the present work . . . . . . . . . . . . . 11

2 DIFFERENT OBSERVATIONAL TECHNIQUES TO STUDY COMETS

19

2.1 Photometry (Optical) . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

2.2 Spectrometry (Optical) . . . . . . . . . . . . . . . . . . . . . . . . . 22

2.3 Polarimetry (Optical) . . . . . . . . . . . . . . . . . . . . . . . . . . . 242.4 Observations at other wavelengths . . . . . . . . . . . . . . . . . . . . 26

2.4.1 Infrared observations . . . . . . . . . . . . . . . . . . . . . . . 26

2.4.2 Ultraviolet observations . . . . . . . . . . . . . . . . . . . . . 29

2.4.3 X-ray and Radio observations . . . . . . . . . . . . . . . . . . 30

2.5 In situ observation on comets . . . . . . . . . . . . . . . . . . . . . . 30

3 TECHNIQUES OF POLARISATION MEASUREMENT 41

ix



3.1 Use of Stokes parameters . . . . . . . . . . . . . . . . . . . . . . . . . 41

3.1.1 Denition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41

3.1.2 Properties of Stokes Parameters . . . . . . . . . . . . . . . . . 42

3.1.3 Transformation Matrix for the Stokes parameters . . . . . . . 44

3.1.4 Transformation Equations for the Stokes parameters . . . . . 45

3.2 Error in polarisation measurement . . . . . . . . . . . . . . . . . . . 48

3.2.1 Photon Noise . . . . . . . . . . . . . . . . . . . . . . . . . . . 48

3.2.2 Atmospheric scintillation and Seeing . . . . . . . . . . . . . . 49

3.2.3 Motion of Light Beam on Photocathode . . . . . . . . . . . . 50

3.2.4 Unnecessary Reections from Optical Components . . . . . . 51

3.2.5 Variable Sky Background . . . . . . . . . . . . . . . . . . . . . 51

3.2.6 Effective Wavelengths . . . . . . . . . . . . . . . . . . . . . . 52

3.2.7 Zero Point of Position Angles . . . . . . . . . . . . . . . . . . 52

3.3 Different kinds of polarimeters . . . . . . . . . . . . . . . . . . . . . . 53

3.3.1 Efficiency of the Polarimeter . . . . . . . . . . . . . . . . . . . 53

3.3.2 Polarimeters without Rapid Modulation Of the Signal . . . . . 54

3.3.3 Polarimeters with Rapid Modulation Of the Signal . . . . . . 55

4 POLARIMETRIC DATA ANALYSIS USING MIE THEORY 57

4.1 Light Scattering Theory . . . . . . . . . . . . . . . . . . . . . . . . . 57

4.1.1 Light scattering by spherical particles : Mie Theory . . . . . . 58

4.2 The in situ dust measurements of Halley . . . . . . . . . . . . . . . . 60

4.3 Polarimetric data of Halley and grain characteristics . . . . . . . . . . 67

5 ON THE VARIATION OF POLARIMETRIC PROPERTIES OFDIFFERENT COMETS 73

5.1 Observed polarimetric variation among comets . . . . . . . . . . . . . 73

5.2 Observed relative abundance of coarser grains in different comets . . 76

5.3 A model to explain the variation . . . . . . . . . . . . . . . . . . . . . 78

5.4 Discussion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 82

6 POLARISATION DATA OF COMET LEVY 1990XX AND AP-

PLICATION OF T-MATRIX THEORY 86



6.1 T-matrix Theory . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86

6.1.1 Theory . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88

6.1.2 Particle shapes and sizes . . . . . . . . . . . . . . . . . . . . . 91

6.1.3 Size Distribution Function . . . . . . . . . . . . . . . . . . . . 91

6.2 Grain characteristics of comet Levy 1990 XX . . . . . . . . . . . . . . 93

6.2.1 Using Mie Theory . . . . . . . . . . . . . . . . . . . . . . . . . 94

6.2.2 Using T-matrix Theory . . . . . . . . . . . . . . . . . . . . . . 95

6.3 Discussions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 96

7 POLARIMETRIC STUDIES OF DARK CLOUDS 103

7.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1037.2 The statical distribution of the degree of polarisation and position

angle in a given cloud . . . . . . . . . . . . . . . . . . . . . . . . . . . 105

7.3 Observed polarisation and ambient physical conditions in the cloud . 110

7.3.1 The dependence of observed polarisation on dust and gas tem-

pera ture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110

7.3.2 The dependence of polarisation on the turbulence in the cloud 118

7.3.3 The dependence of direction of polarisation vector on temper-ature and turbulence . . . . . . . . . . . . . . . . . . . . . . . 123

7.4 The spatial distribution of the polarisation and position angle values 125

7.4.1 A simple model for the polarisation introduced by the cloud . 125

7.4.2 A model for the transmission coefficients of the cloud: . . . . . 128

7.4.3 Fitting the observed polarisation for radial distance from cloud

centre . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 129

7.5 Conclusions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 134



List of Figures

1.1 A Suspected cometary interplanetary dust particle. . . . . . . . . . . 9

3.1 Parameters dening the polarisation of a simple wave. . . . . . . . . . 43

4.1 Log of grain radius (s) against the log of differential spatial density

(N (s)) as obtained from Lamy et al. (1987) for comet Halley. . . . . 64

4.2 The observed and expected polarisation values of comet P/Halley at

λ = 0 .365µm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 69


λ = 0 .484µm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70


λ = 0 .684µm. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 71

5.1 Log of perihelion distance against log (−g), where g is the relative

abundance of coarser grains . . . . . . . . . . . . . . . . . . . . . . . 81

6.1 The observed and expected polarisation values (emerging out from

Mie theory) of comet Levy 1990XX at λ = 0 .485µm. . . . . . . . . . 97

6.2 The observed and expected polarisation values (emerging out from

T-matrix theory) of comet Levy 1990XX at λ = 0 .485µm. . . . . . . 98

6.3 Comparison of Mie theory and T-matrix theory results at λ = 0 .485µm. 99

7.1 Histogram showing the number ( N stars ) distribution of stars having

Rice corrected polarisation ( price ) values in different ranges for various

clouds. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 108

7.2 Histogram showing the number ( N stars ) distribution of stars having

position angle (θ) values in different ranges for various clouds . . . . . 109

xii



7.3 The average of observed polarisation ( pav ) versus T 1(= 1√T g( 1

T d − 1T g ))

for various clouds. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 114

7.4 The average of observed polarisation ( pav ) versus T 2(= T d(T g + T d ) ) for

various clouds. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 115

7.5 The log of average of observed polarisation ln ( pav ) are plotted against

the turbulence ∆ V for various clouds. . . . . . . . . . . . . . . . . . . 116

7.6 The dispersion in the direction of polarisation vectors ( σθ) are plotted

against gas temperatures ( T g) for different clouds . . . . . . . . . . . 117

7.7 The dispersion in the direction of polarisation vectors ( σθ) are plotted

against amount of turbulence (∆ V ) for different clouds . . . . . . . . 120

7.8 The average of observed polarisation ( pav ) are plotted against variance

(σθ) in the direction of polarisation vector. . . . . . . . . . . . . . . . 121

7.9 The average of observed polarisation ( pav ) are plotted against |θG −θav |122

7.10 A model for cloud with the light from background star passing through

it. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 127

7.11 Observed Polarisation versus radial distance plot for the clouds CB3,

CB25, Cb39 and CB52. . . . . . . . . . . . . . . . . . . . . . . . . . . 130

7.12 Observed Polarisation versus radial distance plot for the clouds CB3,

CB25, Cb39 and CB52. The curves joining the , represent our

proposed model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 131



List of Tables

4.1 The log of grain radius (s) and log of differential spatial density ( N (s))

as derived from Lamy et al. (1987). . . . . . . . . . . . . . . . . . . . 65

4.2 The (n, k ) values obtained by previous authors and in the present

work, for comet Halley at different wavelengths. . . . . . . . . . . . . 68

5.1 The ‘relative abundance of coarser grains’ ( g) for different comets

along with their orbital parameters . . . . . . . . . . . . . . . . . . . 77

7.1 For various CB clouds, the number of stars, average polarisation, aver-

age position angle, dispersion, dust and gas temperatures, turbulence

, difference

|θG

−θav

|and cloud groups are shown . . . . . . . . . . . 107

7.2 The values of R0 (arc sec), interstellar polarisation p (in %), φ (in

degrees), c, χ 2 are shown. . . . . . . . . . . . . . . . . . . . . . . . . 132

xiv



Chapter 1

INTRODUCTION

In this Chapter, a historical account of the development of cometary science is

discussed. The basic denition of comets, its structure, classication and origin are

discussed. A brief description of the nature of cometary dust is also given. The

comets and their important role in Solar System studies are then discussed. Finally

the objective and the layout of the thesis are presented.

1.1 A brief historical account of Cometary science:Comets have attracted and fascinated the people for more than two thousand years.

Chinese observation in 240 B.C. was the rst listing of comet in recorded history.

The comets spend almost all their time at great distances from the Sun. The

cometary activity starts when the comet approaches the Sun. In some cases it

becomes brighter and spectacular with coma and tail. From the ancient recordsof paintings or drawings of comets on caves, clothes etc., it is evident that ancient

people were fascinated by this celestial object. Also there are observations recorded

by many early astronomers from historical time. Tycho Brahe developed the ideas

about comets by observing the bright comet of 1577 AD with accurate instruments

from various places in Europe and inferred that comets are solar system objects. Ke-

pler in 1619, proposed that comets follow straight lines and they originate outside

the Solar System. Hevelius suggested parabolic orbits in 1668, but Newton argued

1




1.2:Structure of comets: 2

against a parabolic orbit of the comet of 1681. The contribution of Edmund Halley

in comet studies has revolutionised the ideas about comets. Halley for the rst time,

using Newtonian Mechanics, showed that the comets, which had appeared in 1531,

1607 and 1682, are the one and the same comet with a period of about 75.5 years.

He predicted that the same comet would return in 1758. The comet did appear in

1758, as predicted, but unfortunately Halley was not alive to see his glorious predic-

tion. This famous comet was therefore named as Halley’s comet . In 1986, the same

comet again appeared in the Sky (after 1910 apparition) and research workers from

all over the world have studied that historical comet with a great interest. Since

ancient time, some superstitious beliefs like disasters, calamities, tragedies etc are

associated with the appearance of a comet. There were also fears that a comet might

encounter with the Earth and bring disastrous consequences. But advancement of

Science has erased the fear from the people’s minds.

1.2 Structure of comets:Comets are small celestial bodies several kilometers in diameter constituted mainly

of water, ice and rock. Comets are some of the farthest objects in our solar systemand spend almost all their life time at great distances from the Sun. The name

”comet” comes from the Latin phrase Stellae comatae which means hairy stars.

The three major parts of a comet are the nucleus , the coma and the tail . A comet

consists of a compact solid core, known as nucleus, which is few kilometers in size,

far from the Sun and is difficult to observe. The nucleus is the essential part of

a comet because it is the only permanent feature that survives during the entire

life time of a comet. Several attempts have been made to determine the size of

the nucleus (e.g., Delsemme & Rudd, 1973; Sagdeev et al., 1986a; Wilhelm, 1986,

1987; Fernandez et al. 1999; Sekanina 1997a; Kruchinenko and Churyumov 1997).

The nuclear radius of comet Tago Sato Kosoka and comet Bennet as determined by

Delsemme & Rudd (1973) were 2.2 ±0.27km and 3.76 ±0.46km respectively. The

size of the nucleus is so small that it appears as a point source and can’t be resolved

even with the largest telescope. The direct determination of the size of the nucleus

of a comet was made possible by the study of comet Halley. The images taken by



1.3:Classication of comets: 3

the spacecrafts directly gave the projected dimension. Based on three spacecrafts

results (Vega 1, 2 & Giotto), it was then possible to reconstruct the actual three

dimensional shape of the nucleus. From these images, the dimension of the nucleus

of comet Halley was estimated to be 16 ×8×7.5km (Sagdeev et al., 1986; Wilhelm,

1986, 1987). The estimated total surface of the nucleus was about 400 ±80km 2 and

its volume was about 550 ±165km 3 (Keller et al., 1987a). It has been found that

volatiles coming out of the nucleus of a comet are mostly made up of elements like

H, C, N and O (Clark et al., 1986).

At far-off distances from the Sun, comet appears as a faint fuzzy patch of light. This

fuzzy patch of light is a cloud of gas and dust, known as, coma . The coma grows

in size and brightness as it approaches towards the Sun. The diameter of the coma

is much larger and lies in the range of about 10 4 to 105 km. Whenever the comet

approaches the Sun, a tail starts developing and reaches its maximum extent at

about the closest approach to the Sun. The tail of a comet may extend up to about

107 to 108 km. If the comet is sufficiently active, then the gas and dust ejections

take place on a large scale so that two tails may form. One is wide and curved which

is due to scattering of solar light by dust and is known as dust tail ( or Type II

tail). The other is narrow and straight which is caused by ionised gases uorescing

under excitation from ultraviolet solar radiation and is known as ion tail (or plasma

tail or Type I tail). The tail of ionised gases is always directed away from the Sun.

Based on the study of the ion tail of comets, the existence of the Solar wind was

rst postulated (Biermann, 1951).

1.3 Classication of comets:Comets may be of periodic and non-periodic in nature and their orbits can be de-

scribed by conic section. From the knowledge of the eccentricity ( e) of the comet,

the periodicity can be predicted. For periodic comets, e < 1 where as for non-

periodic comets, e ≥ 1. The periodic comets are classied into two categories: (1)

Short period comets and (2) Long period comets. Comets with an orbital period less

than 200 years are known as Short Period comets. These comets are indicated by

a ”P/” before the names (viz., 1P/Halley, 23P/Brorsen-metcalf, 27/P Crommelin



1.4:Origin of comets: 4

etc.). Comets that have period greater than 200 years are called Long Period comets

(viz., Hale-Bopp, Hyakutake etc.). The Short Period comets that have period be-

tween 20 years < T < 200 years, are known as Halley type comets and the comets

that have period (T) < 20 years are known as Jupiter family comets (viz., 2P/Encke,

21P/Giacobini-Zinner, 22P/Kopff etc), because the orbits of Jupiter family comets

are governed by Jupiter’s gravitational eld. Comets have been classied as ’old’

and ’new’, based purely on their orbital characteristics. Comets that have made

several perihelion passages around the Sun are generally termed as ’old’ and those,

which are entering for the rst time, are called ’new’. If the direction of the comet’s

motion is same as that of the Earth’s motion, it is said to have a direct orbit . If

they are in opposite directions, the comet is said to have a retrograde orbit .

1.4 Origin of comets:There are many ideas and hypothesis about the origin of comets. Kant (1755)

included the existence of comets in the same way as the planets in his nebula hy-

pothesis for the formation of the Solar System. Laplace suggested comets to be

extra-solar in origin in his cosmogony of the protosolar nebula. It was Opik (1932)who rst suggested that a cloud of comets surrounds the Solar System. This idea

was strengthened by Dutch astronomer Jan Hendrick Oort (1950). Oort showed that

a plot of the number of comets (about 19 long period comets at that time) versus

the reciprocal of semi major axis, 1a (equivalent to orbital energies) of the original

orbit gave a sharp peak near zero (,i.e., nearly parabolic orbits). The sharp peak

near zero value of 1a can not be due to chance but represents the real characteristic

property of comets. Therefore most of the comets must have come into the Solar

System for the rst time and these comets are generally called new comets. The

comets, Oort, studied appear to come from a distance between 40,000 and 100,000

AU from the Sun. Thus Oort recognised a cloud of comets around the Sun at this

distance but still gravitationally bound to it. This great reservoir of comets is gen-

erally known as Oort Cloud . The present day calculation shows that Oort cloud

may contain 10 12 comets. Due to perturbation of nearby passing stars, 5 to 10%

of comets leave the Oort cloud forever and some other enter the planetary system.



1.4:Origin of comets: 5

Among these some may happen to come close to Sun and get detected as observable

comets. Sometimes comets may come from another population of comets from a

region, which is believed to contain 108 to 1010 comets in the ecliptic plane beyond

the orbit of Neptune between 30 and 50 AU. This region is known as the Kuiper

Belt . About 200 long period comets have been studied using more accurate and

high precision data available in recent years (Marsden et al., 1978). The period cor-

responding to the peak value of 1a , as observed by Oort, is about 4 ×106 years and

the mean aphelion distance ∼50, 000AU. These distances are almost comparable to

the distances of nearby stars.

The age of a comet is generally measured by the reciprocal of the semi major axis, i.e.,

a− 1. New comets coming from the Oort cloud for the rst time have a > 104 AU or

(1/a ) < 100×10− 6 AU− 1. With successive passages the orbit shrinks gradually due

to planetary perturbations and hence the value of (1 /a ) becomes larger and larger.

Therefore statistically, large values of (1 /a ) means that the comet has gone through

many times in the orbit. Consequently, the increasing value of (1 /a ) corresponds to

higher value of time lapsed since the rst approach to the Solar System. In other

words, (1/a ) gives a measure of the comet’s age.

The dirty snowball model put forward by Fred Whipple (1950), suggests that the

comets are essentially composed of water. The results obtained from the observation

of different comets ensured the evidence of water vapour as the main constituents

in cometary gases, proved this to be correct. When the comets are far from the Sun

(≥ 7AU ), there is very little activity on the cometary nucleus (Prialnik and Dina,

1997). As comet approaches the Sun, the Sun’s radiation heats up the nucleus, then

the temperature of the nucleus increases and ices close to the surface are sublimated

releasing the gas and dust into space, often violently. Observations on comets show

that the volatile fraction is a mixture of molecules comprising of mainly H, C, N, O

and S. These elements were the most abundant in the primitive solar nebula. Also

the study based on the isotopic ratio of 12C/ 13C in many comets gives a value ∼90

(Vanysek and Rahe, 1978; Lambert and Danks, 1983; Jaworski and Tatum, 1991;

Wyckoff et al., 1993 etc.) which is same as the solar system value. The results

suggest that the cometary materials and the Solar System materials are similar in



1.5:The nature of Cometary Dust: 6

nature.

The formation of comets in the inner Solar System is highly unlikely. Because, the

presently known chemical compositions of comets require a temperature at the time

of formation to be quite low (100K ) to keep the volatiles like H2O, CO2, CO, NH3

and CH 4 from evaporating. This led to the other possibility that the comets were

formed in the outer parts of the nebula that formed the planets. The chemical

composition of the Solar System bodies can roughly be divided into three classes

depending upon the characteristics of the elements present in them. As for example,

hydrogen, helium and other noble gases stay in gas phase even at low temperature,

ice melts at moderate temperature and lastly the terrestrial materials like Si, Mg

and Fe melt at higher temperature (Whipple, 1972). It has been found that Jupiter

and Saturn were formed mostly of the original solar material like the Sun while

Uranus, Neptune and Comets were formed in the colder region which account for

the icy material. Therefore, the above hypothesis suggests that comets were formed

beyond Saturn.

1.5 The nature of Cometary Dust:The spectacular view of a bright comet is mostly caused by a cloud of micrometer

sized dust particles present in coma. Dusts in comets consist of a major part of

the non-volatile material. Drago in 1820 recognised that the light from a comet is

mostly scattered sunlight. Bessel (1836) revolutionised the idea on cometary dust

by observing the coma of Halley’s comet at its 1835 apparition and developed a

mathematical theory to explain the structure of the tail and its observed direction

away from the Sun. Bessel introduced a repulsive force opposing the force of solar

gravity which later was identied as the Solar Radiation Pressure (Arrhenius, 1900;

Schwarchild, 1901). In order to understand the formation of dust tails, the concept

of Syndynes (or Syndynames ) and Synchrones (or Isochrones ) were introduced by

Bredichin in 1903. Let us rst consider a nucleus constantly releasing particles with

a certain radiation pressure parameter β and with zero speed relative to the moving

nucleus. The particles are pushed back by the radiation pressure and will form a

line called Syndyne. The Syndyne is the locus of dust particles of the same β at a




certain observation time t0, emitted from the nucleus with zero relative velocity at

different times ( t0 −t), where t is the emission time of the particle relative to the

time of observation. In a Syndyne, the relative emission time, t, of the particles

increases with distance from the nucleus. It is located in the plane of comet orbit,

because the particles experience a central force. Moreover, Syndynes leave the comet

head in the antisolar direction. Generally, the initial velocity of the dust particles

is not zero but has a certain value vd. Correspondingly, a Synchrone is dened as

the locus of the particles of different β emitted at the same time, i.e., consisting of

particles of the same relative emission time , t. Synchrones don’t leave the comet in

the antisolar direction but lag behind it in the opposite sense of the comet’s orbital

motion by an angle dependent on the Synchrone’s age.

Our knowledge of cometary dust comes from polarimetric studies of comets, remote

observation of IR spectral features and the in situ measurement of comets. The

polarisation measurement of the scattered radiation gives valuable information about

the shape, structure and sizes of the dust particles. The appearance of bright comets

Arend-Roland 1957 III and Mrkos (Liller, 1960) gave a good opportunity for making

the rst polarisation measurements. For comets Bennett 1970 II (Bugaenko et

al., 1973) and Kohoutek 1973XII (Bugaenko et al., 1974; Noguchi et al., 1974),

an increase of polarisation with wavelength was reported, while for some others

like comets West (Kiselev & Chernova, 1978), Austin (Sen et al., 1991; Eaton et

al., 1992; Chernova et al., 1993) & Churyumav-Gerasimenko (Tholen et al., 1986),

neutral polarisation in the visible was reported. Many investigators (Bastien et al.,

1986; Kikuchi et al., 1987, 1989; Lamy et al., 1987, Le Borgne et al., 1987; Mukai et

al., 1987; Sen et al., 1991a, 1991b; Chernova et al.; 1993 Joshi et al., 1997; Kiselev &

Velichko, 1998; Ganesh et al., 1998; Manset & Bastien, 2000 etc.) have studied linear

and circular polarisation measurements of several comets. These studies enriched

further the knowledge about the dust grain nature of comets.

Before the in situ analysis of cometary dust was possible in 1986, its composition

was inferred from meteor spectra and laboratory analysis of interplanetary dust

particles (IDP) thought to be related to comets (Millman, 1977; Rahe, 1981). But,

the in situ measurement of Halley, gave us the rst direct evidence of grain mass




distribution (Mazets et al.,1987). Lamy et al. (1987) analysed the data for comet

Halley from spacecrafts VegaI, Vega II and Giotto. The important information

about the chemical composition of dust particles in comet Halley has been obtained

from the dust impact mass analyzer PUMA 1 and 2 on Vega and PIA on Giotto

spacecrafts (Kissel et al., 1986 a, b; Mazets et al., 1987; Lamy et al, 1987). The in

situ measurement of comet Halley indicated three classes of particles:

(1) The lighter elements H, C, N and O indicative of organic composition of grains

called ’CHON’ particles (Clark et al., 1986),

(2) Carbonaceous chondrites of Type I (C I chondrites) and

(3) Mg, Si and Fe, called silicates .

The CHON to silicate ratio was noted to change considerably during the yby,

probably reecting dust jets ejected from different locations on Halley’s nucleus.

Therefore, the comet Halley grains were found to be essentially composed of two

end member particle types - a silicate and a refractory organic material (CHON) in

accordance with the IR observations.

The infrared measurement of comets has provided useful information on the physical

nature of cometary dust grains. Spectral features at 10 µm wavelength allowed the

identication of silicates in comet dust. Another silicate feature at 20 µm also

appears to be present in many comets. The wavelength and shapes of these feature

provide important information for the identication of the mineral composition (

Wooden et al., 1997; Hanner 1999; Wooden et al, 1999; Hayward et al., 2000 ).

There is another very important means available to know the nature of cometary

dust. The dust particles released by comets, are believed to contribute to the pop-

ulation of interplanetary dust particles (IDP), often get collected at high altitudes

of the Earth’s atmosphere. Various methods have been used for the collection of

these particles based on recoverable rockets, balloons and aircrafts. The particles

collected from these ights are subjected to thorough laboratory investigation. If

the IDPs are traced to be of cometary origin, then it would be a powerful tool

to study the morphological, structural and chemical properties of cometary grains.

Laboratory studies have shown that majority of the collected IDPs fall into one of

the three spectral classes dened by their 10 µm feature proles. These observed



1.6:The comets and its important role in Solar System studies 9

proles indicate the presence of olivine, pyroxene and layer lattice silicates. This

is in agreement with the results obtained from Vega and Giotto mass spectrome-

ter observations of comet Halley (Lamy et al., 1987). Mg-rich silicate crystals are

also found within IDPs and are detected through cometary spectra (Hanner et al.,

1999; Wooden et al., 1999). It has been estimated that comets contribute about two

thirds of the IDPs, with the remainder coming from asteroid collisions and crating

events (Boice and Huebner, 1999). As cometary grains are characterised by porous

structures of carbonaceous and silicate aggregates, it is therefore inferred that these

IDPs are originated from comets.

Figure 1.1: A Suspected cometary interplanetary dust particle. This dust particle is highly porous. It is apparently a random collection of sub-micron silicate grains embedded in a carbonaceous matrix. Samples of these grains have been recovered inthe Earth’s atmosphere by high-ying research aircraft. (Courtesy of D. Brownlee,University of Washington.)



1.6:The comets and its important role in Solar System studies 10

1.6 The comets and its important role in Solar

System studies

According to the widely accepted current theories, comets were debris left overfrom the buildings of the outer most planets. The cometary material must be

of interstellar origin from which the Sun and the planetary system evolved. If the

comets were formed along with other Solar System bodies about 4.5 billion years ago,

they would have the same composition as that of the Solar System material. Again

if the comets were formed more recently, they would have a different composition

reecting the contemporary interstellar abundances. So, it is necessary to know the

nature of the primordial cometary particles. The method which can give informationabout the possible nature of the primordial cometary materials and the time scale

or the age is the study of isotopic ratios of various elements. Actually, the relative

abundances of different isotopes preserve the life history of the formation process and

hence help in understanding the nature of the original material. Recently most of the

measurements referred to the isotopic ratio 12C/ 13C in comets. The isotopic ratio

of 12C/ 13C has been analysed extensively for various objects in the Solar System

and in the interstellar medium. The study based on the isotopic ratio of 12C/ 13C in

many comets give a value∼90 (Vanysek and Rahe, 1978; Lambert and Danks, 1983;

Jaworski and Tatum, 1991; Wyckoff et al., 1993 etc.) which is same as the solar

system value. Other isotopic ratios were determined from in situ measurements

of comet Halley and their values are roughly in accordance with the Solar value.

These results suggest that the cometary materials and the Solar System materials

are similar in nature. Therefore, the study of comets will give the information about

the least-processed and primordial materials of original Solar nebula, from which the

present day Solar System has been formed some 4.5 billion years ago.

The study of comets is also important to know the origin of life on Earth. The

standard hypothesis for the origin of life, rst outlined by Oparin (1924, 1938) and

Haldane (1928), begins with the biological production of organic materials. As all

life on Earth is composed of organic materials, the elements C, H, N, O, S and P are

beleived to be essential for all living systems. Miller (1953) did an experiment and

showed that when gaseous mixture of NH 3, CH4 and H2O is subjected to an electric



1.7:The Objective and Layout of the present work 11

discharge, it produced several kinds of organic molecules including amino acids. This

suggests that the same phenomenon has been taken place in the early stages of the

Earth leading to formation of life on Earth. All the elements C, H, N, O, S and P,

essential for living system, have been detected in comets (Clark et al., 1987; Langevin

et al., 1987b; Jessberger et al., 1988). The energy source in the comets could be

Solar wind, Solar UV radiation and cosmic rays. So, there may be important role for

comets in the process of chemical evolution which nally led to formation of life on

Earth. Other studies indicate that the early Earth’s atmosphere contained mostly

CO2, H2O and N2, which make it difficult for the formation of organics (Walker,

1977; Pollack & Yung, 1980; Levine 1985a). The existing observations show that

the amount of organics in the Solar System objects seems to increase with distance

from the Sun. This suggests that the organics necessary for chemical evolution are

found in the outer Solar System, whereas water, an essential ingredient for the life

formation, is found in the inner Solar System. This led to the suggestions that the

organics might have been transferred from outer to inner regions of the Solar System

by some means, possibly through comets. Thus comets may have taken important

role for the formation of life on Earth ( Sen and Rana 1994).

1.7 The Objective and Layout of the present workThe objective of the present work is to study the dust grain properties of different

comets. The theory of scattering of plane EM waves is basic to the study of dust

grains of comets. Several scattering theories ( e.g., Mie theory, T-matrix theory,

etc.) are used to analyse the polarimetric data of comets. In the present work, the

distribution of intensity and the polarisation of different comets have been studied

using Mie theory. Also, the polarimetric data of comet Levy 1990XX has been

analysed using T-matrix theory. One of the major objectives, is to explore the

causes behind the observed variation in polarimetric properties of different comets.

Further, the polarimetric properties of light coming from stars background to sev-

eral dark clouds have been also studied. Some of these clouds are undergoing star

formation processes. Therefore, the polarimetric study was aimed at understanding

this complex process.



1.7:The Objective and Layout of the present work 12

The layout of the thesis includes following chapters:

1. Introduction

2. Different Observational Techniques to study comets

3. Techniques of polarisation measurement

4. Polarimetric data analysis using Mie theory

5. On the variation of polarimetric properties of different comets

6. Polarisation data of comet Levy 1990XX and application of T-matrix theory

7. Polarimetric studies of dark clouds

As already discussed, the rst chapter contains an overview of Cometary Science in

general. In this chapter, the basic denition of comets, its structure, classication

and origin are discussed. A brief description of the nature of cometary dust is also

discussed. The comets and their important role in Solar System studies are then

discussed.

The second chapter will contain information on several methods, e.g., Photometry,

Spectrometry, Polarimetry which are used in the optical region for the study of

comets. Besides these, techniques of measurement at other wavelengths will also be

discussed. The in situ space-craft measurement of comets will be discussed in this

chapter.

The third chapter will contain a brief overview of polarisation measurement tech-

niques. The concept of Stoke’s parameters and error in polarimetric measurement

are discussed. The use of polarimeter are also discussed here.

The fourth chapter will contain different light scattering theories (mainly Mie) and

techniques (numerical methods) to calculate theoretically expected polarisation val-

ues.

The fth chapter will contain the study of variation of polarimetric properties of

different comets. In this chapter, a model will be proposed to explain this variation

in terms of aging of cometary dust by solar radiation.





References 14

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Chapter 2

DIFFERENT OBSERVATIONAL

TECHNIQUES TO STUDY

COMETS

In this chapter Photometric, Spectrometric and Polarimetric (Optical) measure-

ments on comets are discussed. Observations at other wavelengths (e.g., Infra red,

Ultra Violet, X-ray and Radio) are then discussed. Finally in situ observations of

comets are presented.

2.1 Photometry (Optical)The photometry of celestial objects is of fundamental importance to astronomy. The

basic goal of astronomical photometry is to measure the light ux from a celestial ob-

ject at several wavelengths. The problem begins when different observers are using

different light detectors and telescopes, and try to compare or combine their data.

Thus the obvious rst step towards a uniform data set will be to have all observers

use the same kind of detectors. It is also valuable to isolate and measure certain

portions of the spectrum containing features that indicate physical conditions of the

celestial bodies (stars, comets etc.). This can be achieved by using a detector with

a broad spectral response with individual spectral regions isolated by lters trans-

mitting only a limited wavelength interval to the detector. Every observer should

19

Himadri Sekhar Das




2.1:Photometry (Optical) 20

match the detector and lters as closely as possible to a common system. Thus

a third and a nal component becomes a necessity: standard stars. Observations

of the same non -variable stars, of known magnitudes and colours, will allow each

observer to determine his (her) own coefficients. It is then possible to measure the

magnitudes of any celestial objects and transform the results to a common photo-

metric system. Thus by specifying the detector, lters and a set of standard stars,

photometric system can be dened (Henden & Kaitchuck, 1982). Most estimates

of comet magnitudes have been done by visual or photographic methods. However,

Charge Coupled Device (CCD) observations of comets have become of widespread

use in the post Halley era.

Comets in general possess a continuum in the visible region of the spectrum. The

strength of the continuum varies from comet to comet and with the heliocentric

distance for the same comet. The observed continuum is attributed to the scatter-

ing of the solar radiation by the dust particles. Therefore, the dusty comets should

have a strong continuum. But at certain wavelengths, however, the continuum fea-

tures are contaminated due to the cometary molecular line emissions. Therefore,

the continuum has to be corrected for these emission features or a spectral region

has to be selected where the emission features are absent or minimal. Since the last

apparition of comet Halley (1985-86), observers have been using a set of bandpass

interference lters, centered at λ = 3650, 4845, 6840A, (with FWHM 80 A, 65A and

90A respectively) to avoid contamination by line emission. Such lters, commonly

known as IHW (International Halley Watch) lters have made comparison of pho-

tometric data of various comets easy. IHW had also suggested an additional set of

ve narrow band interference lters to study molecular emissions: C 2 (5140 A), C3

(4060 A), CN (3871 A), OH (3090 A), CO+ (4260 A) bands.

The photometric study of the comets will be helpful to measure the nuclear size of

comets at large heliocentric distances (Svoreˇn, 1982; Larson, 1980; Cochran et al.,

1980; Cowan & A’Hearn, 1982 etc.). The brightness of a comet depends upon three

factors : (i) the distance r from the Sun to the comet, ( ii ) the nature of the comet

and ( iii ) the distance ∆ from the comet to the Earth. The expected brightness of a



2.1:Photometry (Optical) 21

comet I, can be written as

I =I o

r 2∆ 2 φ(α) (2.1)

where, φ(α) is the phase function, I 0 is the constant of proportionality, usually taken

to be the brightness of the comet at r = ∆ = 1 AU. It has been observed that the

power of r is greater than 2 (Jacchia, 1974).

Without invoking the role of phase function one may write:

I =I o

r n ∆ 2 (2.2)

The above equation can be written in terms of magnitudes as

m = m0 + 5 log ∆ + 2 .5n log r (2.3)

where m is the total apparent magnitude, m0 is the absolute magnitude which

corresponds to r = ∆ = 1 AU. The study of large number of comets has given a

good idea about the variation of brightness with heliocentric distance r as well as the

mean value of n. The study based on photometric data for more than 200 comets

(Whipple, 1991) reveals that the mean value of n lies in the range 2.4 < n < 5.

Since the value of n is uncertain, the equation (2.3) can be written in a simpliedform as

m = 5 log ∆ + m(r ) (2.4)

where,

m(r ) = m0 + 2 .5n log r

From the observed light curve, the value of m(r ) can be calculated from equation

(2.4) as a function of the time from the perihelion passage. Festou (1983) observed

comet Crommelin (1984 IV) and calculated the expected brightness using equation

(2.4). The brightness of several comets has been studied using equation (2.4).

The gas production rate of a comet can also be determined from the knowledge of the

observed light curve of the comets. The light curve of a comet gives the variation

of apparent brightness as a function of the heliocentric distance. In general, the

observed brightness in the visual region is mainly due to the continuum and the

Swan bands of the C 2 molecule. The continuum is made up of scattering by the

dust particles in the coma as well as the reection from the nucleus. Since H 2O



2.2:Spectrometry (Optical) 22

is the most abundant molecule in a comet, the cometary activity is basically given

by the production rate of hydrogen, Q H (Newburn, 1981; Divine et al., 1986). The

results for comet Bradeld (Budzien et al., 1994) indicate the dependence of the

H2O production rate with heliocentric distance as r − 3.8 to r − 4.4. For comet Austin

1990V, the variation is between r − 1.8 to r − 2.8. The study of several comets has

shown a variation of the production rate of H 2O with the heliocentric distance from

that of r − 2 dependence (Despois et al., 1981). The results for the production rates

of CN, C2, C3, CH etc. (Swift & Mitchell, 1981; Cochran, 1985; Schleicher et al.,

1987) indicate to a rst approximation that comets of various types, dynamical ages

and morphologies have very little variation in their chemical composition. From the

study of several comets, it has been suggested that even though the lines of C 2, CN

and others dominate the visual spectral region, their production rates are lower by

a factor of 100 or so compared to that of H2O or H.

2.2 Spectrometry (Optical)Spectrometric study of comets is one of the active and important areas to study.

Various cometary phenomenon can be understood from the identication of thespectra of comets. Several transitions were observed rst in the cometary spectra

before being studied in the laboratory. The well known case is the bands of the ion

CO+ , generally called the Comet - Tail system. Other examples are the bands of

C3 and H2O+ . The observations carried out in the visual spectral region of around

3000 to 8000A have been the main source of information for the study of cometary

atmosphere. Based on the spectra in the visible region, it is possible to arrive at

some general pattern regarding the main characteristic features of the spectra of

comets.

For heliocentric distances, r ≥ 3 AU, the spectrum mainly comprises of the con-

tinuum radiation arising due to the solar radiation scattered by the dust particles

present in the cometary atmosphere. As comet approaches Sun, the emission lines

of the various molecules appear. The molecular bands rst to appear are those of

CN at r

∼

3 AU followed by the emission from C3 and CH. Thereafter, the emission

from C2, OH, NH and NH2 appear in the spectrum. They are often strong enough



2.2:Spectrometry (Optical) 23

to reveal their structure (Swings & Haser, 1956; Arpigny et al., 1995). The spectra

of comet Encke showed the Swan band sequences corresponding to ∆ v = −1, 0, +1

of the C2 molecule, whose wavelengths lie around 5635A, 5165A and 4737A respec-

tively. The spectra of comet Halley taken at a spectral resolution of 0.07 A beautifully

shows the rotational structure of the (0,0) Swan Band of the C 2 molecule (Lambert

et al., 1990). Since the Swan bands of the C 2 molecule dominate the spectrum in

the visual region, to a rst approximation, it also determines the visual diameter of

the head of the comet.

The emission due to C 3 molecule has a broad feature extending from 3950 to 4140

A, with a strong peak around 4050 A. The identication of C 3 feature in comets

was difficult as the laboratory analysis was not available. Various transitions of

the CN molecule, both at the red ( λ ∼7800A- 1 µm) and the violet ( λ ∼3600

- 4200A) wavelengths have been identied. The rotational structure of CN band

is well resolved (Whipple, 1978). The lines of H2O+ (λ ∼5500 −7500A) were

identied for the rst time in comet Kohoutek (Huppler et al., 1975). The bands

of CO+ around λ ∼(3400 - 6300 A) have been observed in many comets. The

sodium D-lines at 5890 and 5896 A, can show up for r

≤1.4 AU. The in situ mass

spectrometer studies of comet Halley has given lot of new information about the

species present in the coma (Huebner et al., 1991). The good quality spectra that

exists for comet Halley has shown a large number of unidentied lines (Crovisier &

Schloerb, 1991). Several conclusions have been drawn from the observed atomic and

molecular spectra of comets (Huebner et al., 1991). Some of these are:

(i) The molecules detected are composed of the most abundant elements in the Solar

System, namely H, C, O and N.

(ii ) Most of the species detected are organic, indicating the importance of carbon,

similar to the case of interstellar molecules.

(iii ) The presence of NH and NH2 implies that NH 3 should be present.

(iv) Methane (CH 4) is tentatively identied.

(v) The presence of CO2 in comets was inferred indirectly from the presence of CO +2 .

But the direct determination of CO 2 came from the Infra red observation of comet

Halley .



2.3:Polarimetry (Optical) 24

The study of the isotopic abundances in comets has attracted many investigators.

Since comets contain the most abundant elements, namely H, C, N and O, do have

many isotopes. Therefore a comparison of the isotopic ratios of these elements in

different kinds of objects will reveal the history of the whole evolutionary process.

Also the detection of several complex molecules in comets has given important in-

formation that the cometary material and the interstellar material could be very

similar in nature. The study based on the isotopic ratio of 12C/ 13C in many comets

give a value∼90 (Vanysek and Rahe, 1978; Lambert and Danks, 1983; Jaworski and

Tatum, 1991; Wyckoff et al., 1993 etc.) which is same as Solar System value. The

other measured isotopic ratios of 16O / 18O

∼

450 and 32S / 34S

∼

22 from in situ

mass spectrometry are also consistent with the solar values of 500 & 23 respectively

(Langevin et al., 1987a; Jessberger et al., 1988 a, b). These results suggest that the

cometary materials and the Solar System materials are essentially the same.

2.3 Polarimetry (Optical)Cometary polarimetry has always been considered a powerful tool in the study of

cometary dust. The polarimetric studies of comets can give important informationabout the nature and composition of the cometary particles. Comets were among

the rst astronomical objects recognised as polarisers of light. Arago (1855) was

the rst to discover the existence of polarisation in comets when visually observing

the comets 1819 II and 1835 III. Wright (1881) found maximum values of P to

be as high as 23% and 13.8% for comets 1881 III and 1881 IV respectively, and

noted rapid changes in P for both comets. The contemporary stage of polarisation

investigations begin with the work of Ohman (1939, 1941). Ohman supposed two

different polarisation mechanisms to act in comets: ( i) polarisation by resonance

uorescence of molecules and (ii ) polarisation due to scattering of sunlight by dust

grains.

Comets in general possess a continuum in the visible region of the spectrum. But at

certain wavelengths, however, the polarisation features, are contaminated due to the

polarisation present in the cometary molecular line emissions. As already discussed

in Section 2.1, since the last apparition of comet Halley (1985-86), observers have



2.3:Polarimetry (Optical) 25

been using a set of lters, centered at λ = 0 .365, 0.484, 0.684µm, to avoid contam-

ination by line emission. Such lters, commonly known as IHW lters have made

comparison of polarisation data of various comets easy.

Linear and circular polarisation measurement of several comets have been studied

by several investigators over last fty years (Hoag, 1958; Bappu & Sinvhal, 1960;

Bappu et al., 1967; Bucher et al., 1975; Kiselev & Chernova, 1978, 1981; Osherov,

1975; Michalsky, 1981, Bastien et al., 1986; Kikuchi et al., 1987; Le Borgne et al.,

1987; Sen et al., 1991a, 1991b; Chernova et al., 1993, Joshi et al., 1997; Kiselev

& Velichko, 1998; Ganesh et al., 1998; Manset & Bastien, 2000 etc.). Actually,

the observed linear polarisation of comets is generally a function of ( i) incident

wavelength ( λ), (ii ) Scattering angle ( θ) (1800 - Phase angle), ( iii ) the geometrical

shape and size of the particles and ( iv) the composition of the dust particles in terms

of complex values of refractive index m(= n −ik).

Phase angle dependence of cometary polarisation has been studied by several in-

vestigators in past. Investigated comets were West 1976 VI, Chernykh 1978 IV,

Ashbrook - Jackson 1978 XIV, Meier 1978 XXI, Churyumov - Gerasimenko 1982

VIII etc. (Kiselev & Chernova, 1978, 1981; Dobrovolsky et al., 1980). Observations

of comets Arend-Roland 1957 III, Mrkos 1957 V (Bappu & Sinvhal, 1960), Ikeya

- Seki 1965 VIII (Bappu et al., 1967), Tago - Sato -Kosaka 1969 IX (Wolf, 1972),

Bennett 1970 II (Bugaenko et al., 1973; Kharitonov & Rebristyi, 1973), Kohoutek

1973 XII (Bugaenko et al., 1974; Noguchi et al., 1974), West 1976 VI (Kiselev &

Chernova, 1978), showed that, in the visual domain, the polarisation increases with

increasing wavelength. The polarimetric observation of comet Halley has enriched to

a very large extent our knowledge in cometary science (Bastien et al., 1986; Kikuchi

et al., 1987; Le Borgne et al., 1987; Sen et al., 1991a; Chernova et al., 1993). Analy-

sis of these polarisation data reveal the nature of the cometary grains, which include

size distribution, shape and complex refractive index of cometary grains. The in-

situ space craft measurement of Halley, gave us the rst direct evidence of grain

mass distribution ( Mazets et al. 1987). Lamy et al (1987) compared the data from

various space crafts like Vega I, Vega II and Giotto, and arrived at grain size distri-

butions for Halley, for various bulk densities. From the work of Mazets et al (1987),



2.4.1:Infrared observations 26

assuming a power law size distribution, one can derive the value of complex refrac-

tive index of cometary grains, using Mie type scattering process ( Mukai et al. 1987,

Sen et al. 1991a). These complex refractive indices can characterise the composition

of cometary grains. Also the study of several other comets like Bradeld 1987XIII

(Kikuchi et al., 1989; Chernova et al., 1993), Levy 1990 XX (Chernova et al., 1993);

Austin 1990V (Chernova et al., 1993; Sen et al., 1991b), Hale-Bopp (Ganesh et al.,

1998; Manset & Bastien, 2000), Hyakutake (Joshi et al., 1997; Kiselev & Velichko,

1998) etc enriched further the knowledge about the comets.

2.4 Observations at other wavelengths2.4.1 Infrared observations

The IR observation of comets can provide another useful method for extracting

important information on the physical nature of the cometary grains. Actually, the

observed IR radiation arises from the re-radiation of the absorbed energy by the dust

particles which depends on the shape, size, texture, temperature and composition of

the dust. It is possible to infer the physical and chemical nature of cometary grains

from a detailed comparison of the cometary IR radiation with the expected IR uxes

based on grain models. The shape and relative strength of the IR emission from a

grain is dependent on the intrinsic properties of the dust (shape, size and composition

etc), as well as the temperature of the grain. Dust grains are primarily heated

through solar radiation and cooled through thermal re-radiation. Other heating and

cooling processes, such as interaction with the solar wind and volatile sublimation are

negligible (Lien, 1990; Lisse et al., 1998). To calculate the temperature of the dustgrains in the coma, it is assumed that the dust grains are in radiative equilibrium

with the solar radiation eld. The equilibrium temperature of the grain is, therefore,

determined by a balance between the absorbed radiation which is mostly in the

ultra violet (UV) and visible regions, and the emitted radiation which is in the far

IR region. Once the temperature of a grain is determined, the ux produced by a

collection of grains of various radii can be easily calculated by assuming a grain size

distribution.




Thus,

F abs (a) = F em (a, T g) (2.5)

where,

F abs (a) = ( Rr

)2 F (λ).Qabs (a, λ ).πa 2dλ (2.6)

and

F em (a, T g) = πB (λ, T g).Qabs (a, λ ).4πa 2dλ (2.7)

where F (λ) represents the incident solar radiation eld at wavelength λ, Qabs (a, λ )

is the absorption efficiency and B(λ, T g) is the Planck function corresponding to

grain temperature, T g. The calculation of the grain temperature involves a knowl-

edge of the size and composition of the grains. Actually, larger grains are cooler than

smaller grains. Smaller grains are superheated (Gehrz & Ney, 1992), compared to

perfectly absorbing conducting spheres of higher radius and at the same heliocentric

distance.

In general, the emission has to be integrated over the size distribution function

characterised by a minimum and maximum grain radii a0 and amax to get the total

IR emission from the grains. Therefore, the total IR emission at the Earth is given

by

F em (λ, r ) =1

∆ 2 a max

a 0

n(a).πa 2.Qabs (a, λ ).B (λ, t g).da (2.8)

where n(a)da represents the relative number of grains in the size interval between

a and a + da, ∆ is the geocentric distance of the comet. However, the grain size

distributions for various comets are not well established in most of the cases. Com-

monly, a power law distribution, n(a)da ∝a− α da is adopted. For many comets,

Hanner(1983) has shown that a modied power law of the form:

n(a) = (1 −a0

a)M .(

a0

a)N (2.9)

provides an adequate model for IR data ranging from 3.5 to 20 µm. In the equation

(2.9), a0 is the minimum grain radius (0.1 µm), N is the slope of the distribution at

large a , and M is related to the radius of the peak of the size distribution (,i.e., the

grain radius at which the grain size distribution rolls over) by

a p = a0 (M + N )N

(2.10)




Typically, 3 .7 < N < 4.2 for comets (Hanner, 1984). For use in equation (2 .9), n(a)

is normalised by the value at the peak of the size distribution, or n(a p).

The IR measurements of comets have provided useful information on the physical

nature of cometary dust grains. The rst IR observations made on comet Ikeya-

Seki in 1965 (Becklin et al., 1966) in the wavelength region of 1 to 10µm showed

clearly that the comet was very bright in the IR wavelength region and its colour

temperature was higher than that of a black body at the same heliocentric distance.

Most of the observations on comets before comet Halley were limited to broad band

IR observations in the spectral region around 2 to 20 µm. The important observation

which gave some clue to the possible nature of the grain was the detection of a broad

10µ emission feature in comet Bennett (Maas et al., 1970). Spectral feature at 10 µm

wavelength allowed the identication of silicates in comet dust. Another spectral

feature at 20 µm also appears to be present in many comets. The wavelength and

shapes of these features provide important information for the identication of the

mineral composition (Wooden et al., 1997, 1999; Hanner 1999, 2003; Haward et

al, 2000). The observations of comet Halley in the 5 to 10µm region obtained on

12 Dec 1985 and 8 April 1986 corresponding to the same heliocentric distance of

1.32AU for pre- and post-perihelion positions agree very well indicating that the

dominant grain material was nearly the same for both the dates (Bregman et al.,

1987; Hanner, 1988). A new emission feature near 3.4µm was rst detected by Vega

I spacecraft in the spectra of comet Halley (Krishna Swamy et al., 1989). This was

conrmed by several ground-based observations (Hanner et al., 1994; Disanti et al.,

1995). The 3.4µm feature is a characteristic of the C-H stretching vibrations and

indicates the presence of some form of hydrocarbons. The IR spectra of comets

suggest that there are two components to the grains - silicates and some form of

hydrogenated carbon. Several physical mechanisms have been suggested to explain

the 3.4µm feature. At small heliocentric distances, the silicate grains are quite hot

and therefore emit a substantial amount of radiation at shorter wavelengths. This

radiation raises the continuum level which makes the 3.4 µm feature weaker. However

at larger heliocentric distances, the silicate grains are cooler and therefore emit less

in the 3.4µm region, which makes the feature appear stronger. Thus the thermal



2.4.2:Ultraviolet observations 29

emission approach can qualitatively explain the observed behaviour of the 3.4 µm.

This demonstrates that the variation of the grain temperature with heliocentric

distance can account for the major changes observed in cometary spectra (Hanner

et al., 1994; Disanti et al., 1995, 1999, 2001).

Several comets display a strong silicate feature with a distinct peak at 11.25 µm,

attributed to crystalline olivine grains: Levy 1990XX (Lynch et al., 1992), Bradeld

1987XXIX (Hanner et al, 1990, 1994a), comet Mueller 1993a (Hanner et al., 1994b),

P/Halley (Bregman et al., 1987; Campins & Ryan, 1989), P/Borrelly and P/Faye

(Hanner et al., 1996).

2.4.2 Ultraviolet observations

Ultraviolet (UV) observations of comets can provide another important method

for the study of both the cometary components: the gas and dust. Since ozone

layer in the Earth’s atmosphere completely blocks the UV radiation shortward of

about 300nm , no ground-based observations are possible. But the use of rockets

and satellites have made it possible to extend the observations into the UV region.

This is the region of the spectrum say, from 1000 to 4000˚A where the abundant

atomic and molecular species have their resonance transitions. Actually, the spectra

of comets taken in the UV region has clearly demonstrated the richness of molecular

emissions in this spectral region.

Comet West in 1976 provided a good opportunity to secure high quality spectra

in the UV region as the comet was quite bright (Feldman & Brune, 1976). Many

molecules like CS,CN + and others were identied for the rst time based on the

spectra of comet West covering the wavelength region from 1600 to 4000 A. Severalstrong emission bands of the S 2 molecule have been identied in the wavelength re-

gion of 2800-3100A based on the beautiful spectra of the comet IRAS-Araki-Alcock

(1983VII) (A’Hearn et al., 1983). The observations made with the orbiting astro-

nomical observatory (OAO -2) satellite in 1970 on comet Bennett (1970II) and on

comet Tago-Sato-Kosaka (1969IX) in the light of the hydrogen Lyman α line at

1216A led to the discovery of a hydrogen halo around the visible coma. This im-

portant observation also led to the realisation that the mass loss rates from comets



2.5:In situ observation on comets 30

are much higher than previous estimates which were based on observations in the

visual spectral region. But the most successful UV satellite to date has been In-

ternational Ultraviolet Explorer (IUE), a joint venture by NASA, ESA (European

Space Agency) and the British Science and Engineering Research Council (SERC),

which has been operating since 1978. The instruments on board this satellite cover

the spectral region from 1150 to 3400A (Feldman, 1982, 1989). It could be used on

comets as faint as 10th Magnitude. Hence IUE satellite has been used extensively

for making observations on many comets, in the UV region and covering a wide

range of heliocentric distances. So far around 40 comets have been observed with

the IUE satellite. They all seem to show similar UV spectra. Observations of comets

Austin(1990V) and Levy(1990XX) at λ < 1200A have indicated the presence of a

feature at 1025.7 A which is a blend of Lyman β line of HI and OI line.

2.4.3 X-ray and Radio observations

The rst ever detection of X-ray from a comet was made with the ROSAT satellite

on March 27, 1996 (IAU 6345). The strong X-ray intensity, primarily of energies

less than 2keV as well as its variation over a few hours was another surprise. X-ray emission from several comets: C/1990K1 (Levy); C/1990 N1 (Tsuchiya-Kiuchi);

45P/Honda-Mrkos-Pajdusakova had also been seen in data obtained with the posi-

tion sensitive proportional counter of ROSAT during the all-sky survey (IAU 6353,

6364, 6366, 6373, 6404). Therefore X-ray emission appears to be the general features

of all the comets.

Radio wavelengths are typically a million times larger than optical wavelengths. The

hydroxyl (OH) radical gives rise to lines in the radio region due to Λ - splitting of thelevels. Radio continuum emission in the cm wavelength region of the EM spectrum

has ben successfully detected from several comets: Kohoutek (1973XII), West (1976

VI), IRAS-Araki-Alcock (1983 VII), and P/Halley (Falchi et al., 1987) etc.

2.5 In situ observation on cometsThe in situ measurement involves the direct analysis of samples taken on board

the probe, e.g., counting of particles, mass spectroscopic analysis of grains or gases,




analysis of the solar wind or magnetometry. The rst in situ measurements were

carried out on comet 21/P Giacobini - Zinner ( 1985 XIII) by the ICE ( Interna-

tional Cometary Explorer) Satellite on September 11, 1985 which passed through

the plasma tail of comet Giacobini - Zinner. Although the spacecraft was not origi-

nally intended for a comet mission, but the space mission was successful in providing

various important data. This mission gave the rst and only measurements of the

density and low energy distribution of the electrons (Coplan et al., 1987). The study

of comet Halley in 1986 was a tremendous success for cometary science. Halley’s

1986 apparition presented an ideal opportunity for cometary scientists to study it.

Halley’s comet was situated almost behind the sun at perihelion passage on 9 Feb

1986, and was therefore very badly placed for earth-based observation. The tele-

scopic observations were thus best carried out before perihelion in April 1986. In

order to study this famous comet thoroughly, scientists of different regions suggested

space exploration of comet Halley.

Five space probes were sent to investigate comet Halley: a European probe: Giotto

(named after the Italian painter Giotto di Bondone); two Soviet probes: Vega1 and

Vega2 and two Japanese probes: Suisei (comet) and Sakigake (Pioneer). All the

encounters took place on the sunward side of the comet. The spacecraft Giotto,

which passed at a distance of approximately 600 km from the nucleus, made the

closest approach to the nucleus. The spacecrafts Vega1 and Vega2 passed at a

distance of around 8000 km from the nucleus. The distances of the closest approach

of the Japanese probes Suisei and Sakigake were around 1 .5×105 km and 7.6 ×106

km respectively. The ICE spacecraft also passed through at a distance of around

0.2 AU upstream of comet Halley later in March 1986. In 1992, the European

probe, Giotto had been subjected to a series of tests and redirected towards a new

less active comet, 26P/Grigg - Skjellerup. The name of the mission was Giotto

Extended Mission ( GEM ) and the yby took place on 10th July 1992. This

mission also helped scientists to know more about comets.

The in situ measurements gave a large number of unexpected results as well as

showed the complexity of the physical processes occurring in coma. These obser-

vations, combined with ground based and satellite observations, covered the entire




range of the electromagnetic spectrum from the far ultraviolet to radio wavelengths

providing the complete set of data available on any comet. These results have dra-

matically increased our knowledge about cometary science. Some of the previously

existing theories and hypothesis have been conrmed by these in situ measurements.

The y-by of ICE spacecraft through comet Giacobini-Zinner and the Giotto space-

craft passing through P/Grigg-Skjerllerup which are short period comets compared

to comet Halley, have also given some important data on these two comets.

The ICE spacecraft, which rst passed through the tail of comet P/Giacobini-Zinner

and last passed through Halley, gave important measurements of the unperturbed

solar wind upstream of the comet. The Giotto probe and the two Vega probes

passed very close by the comet Halley and carried out important measurements.

The three probes were provided with a camera to photograph the nucleus and its

immediate neighbourhood. They also carried several mass spectrometers to study

the chemical composition of neutral gases, ions and cometary grains etc. In addi-

tion to that Giotto probe had a photopolarimeter for studying optical properties of

cometary dust particles. The Japanese probes: Suisei and Sakigake, which ew by

at greater distances from the comet were designed to study the hydrogen envelope

by analysis of its UV radiation in the Lyman α line at 121.5nm , and also to study

the electromagnetic environment of the comet.

The most readily available information on comet comes from ground-based optical

observations of the dust coma and tail. A large number of comets have been ob-

served in this way. The size distribution function of cometary grains has always

been indirectly determined from either their visible scattering light or their thermal

emission. For the rst time, the space missions to comet Halley gave direct access

to study the physical and optical properties of the dust grains. The in situ mea-

surement on comet Halley gave conrming evidence for some of the basic ideas of

gas-phase chemistry. The ion mass spectrometer on board the Giotto spacecraft has

provided important information about the ions present in the coma of comet Halley

to a distance of 1000 km (Huebner et al., 1991). However the in situ detectors

on board of the spacecraft best determined the mass distribution of cometary dust

particles. The spatial densities at a distance of 1000 km from the nucleus of comet





References 34

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Chapter 3

TECHNIQUES OF

POLARISATION

MEASUREMENT

In this chapter, the basic denitions of polarisation in terms of Stokes parameters

are discussed. Then the properties of Stokes parameters, transformation matrix and

transformation equation for Stokes parameters are discussed. Different errors in po-

larisation measurements are then discussed. Finally, different kinds of polarimeters

are discussed.

3.1 Use of Stokes parameters

3.1.1 Denition

Polarised light is most conveniently described by means of four parameters, I, Q,

U, V, which were introduced by Sir George Stokes (1852). We shall consider simple

electromagnetic wave. Let l and r (the letters l and r are the last letters of the

words paralla l and perpendicula r ) be the two mutually perpendicular vectors in a

xed plane perpendicular to the direction of propagation of this wave. They are

so chosen that r×l is in the direction of propagation and l is lying in the plane of

meridian of equatorial coordinate system. The components of the electric vector E

41




3.1.2:Properties of Stokes Parameters 42

of a simple wave in some xed point of space may be represented as a function of

time t of the form (Chandrasekhar, 1950):

E l

= E l0

sin(ωt

− l) (3.1)

E r = E r 0 sin(ωt − r ) (3.2)

where ω is the angular frequency and E l0, E r 0, l and r are constants.

It is obvious from equation (3.1) and (3.2) that the end of the vector E outlines an

ellipse in the l - r plane (Fig 3.1). This means that the plane wave is, in general,

elliptically polarised.

We shall denote θ, by the angle which the long axis of an ellipse makes to the direc-

tion l, and β , by an angle whose tangent is the ratio of the axes of the ellipse. The

stokes parameters describing the simple wave will now be dened by the equations

(Chandrasekhar, 1950):

I = E 2lo + E 2ro = ( Q2 + U 2 + V 2)1/ 2, (3.3)

Q = E 2lo −E 2ro = I cos2β cos2θ, (3.4)

U =

−2E l0E r 0 cos( l

−r ) = I cos2β sin2θ, (3.5)

V = 2 E l0E r 0 sin( l − r ) = I sin2β, (3.6)

The Stoke’s parameter I is simply the intensity of the beam. If we choose another

system of coordinates, I and β remain the same, only θ changes; hence I , Q2 + U 2

and V are invariants with respect to the change of the coordinate system.

3.1.2 Properties of Stokes Parameters

The Stokes parameters describing the actual light are sums of the corresponding

Stokes parameters describing the simple waves of which the light is composed of.

In general, the Stokes parameters characterising the light beam which is a mixture

of several incoherent light beams are the sums of the respective Stokes parameters

characterising these component beams. From this additivity of the Stokes param-

eters results the principle of optical equivalence. This principle states that it is

impossible by any optical analysis to distinguish between two beams characterised

by the same same set of Stokes parameters.



3.1.2:Properties of Stokes Parameters 43

Figure 3.1: Parameters dening the polarisation of a simple wave. The light is coming toward observer and l is lying in the plane of meridian of the equatorial coordinate system and directed towards the northern hemisphere.



3.1.3:Transformation Matrix for the Stokes parameters 44

The most general mixture of light can be regarded as partially elliptically polarised

light. Such light, described by the Stokes parameters I ,Q,U and V , may always be

decomposed into two beams:

1. Natural unpolarised light of intensity I − (Q2 + U 2 + V 2)1/ 2; for this beam

Q = U = V = 0,

2. Fully elliptically polarised light of intensity ( Q2 + U 2 + V 2)1/ 2.

If the intensity of this last beam is much smaller than that of the rst one, the light

may be decomposed into three beams, namely:

1. Natural light of intensity I −(Q2 + U 2)1/ 2 − |V |.2. Fully plane polarised light of intensity ( Q2 + U 2)1/ 2, for which V = 0.

3. Fully circularly polarised light of intensity |V | for which Q = U = 0; V > 0

corresponds to right-handed circular polarisation, V < 0 to left-handed polarisation.

The ratio

P = ( Q2 + U 2)1/ 2/I (3.7)

is called the degree of polarisation while the ratio

P v = |V |/I (3.8)

is called the degree of circular polarisation . The fully plane polarised light is char-

acterised by P = 1, and fully circularly polarised light by P v = 1.

The partially plane polarised light (for which V = 0) may be decomposed into two

beams of fully plane-polarised light. We shall denote by I max the intensity of the

plane polarised component for which the electric vector makes an angle θ to the

direction l, and by I min the intensity of component for which this angle is θ + 90 0.

Now the Stokes parameters for partially plane polarised beam are

I = I max + I min , (3.9)

Q = ( I max −I min )cos2θ = P I cos2θ, (3.10)

U = ( I max −I min )sin2θ = P I sin2θ, (3.11)

3.1.3 Transformation Matrix for the Stokes parameters

Let us consider the simple wave with arbitrary polarisation passing through an

arbitrary optical instrument which produces no incoherent effects so that a simple





3.1.4:Transformation Equations for the Stokes parameters 46

can be described either by its intensity I , degree of linear polarisation p, position

angle θ in the equatorial coordinate system, and degree of circular polarisation q,

or by the Stokes parameters:

I ,

Q (= Ip cos2θ),

U (= Ip sin2θ),

V (= Iq).

(3.17)

The Stokes parameters I , Q , U and V of the light transmitted through a perfect

analyser with the principal plane at position angle φ are connected with Stokes

parameters I , Q, U and V , describing the incident light, by a matrix transformationequation:

I

Q

U

V

=12

1 cos 2ϕ sin2ϕ 0

cos2ϕ cos2 2ϕ 12 sin4ϕ 0

sin2ϕ 12 sin4ϕ sin2 2ϕ 0

0 0 0 0

I

Q

U

V

(3.18)

From this equation we obtain the intensity of the light transmitted through a perfectanalyser

I =12

(I + Q cos2ϕ + U sin2ϕ) (3.19)

The transformation equation for a perfect retarder of retardance τ and optic axis at

position angle ψ is

I Q

U

V

=

1 0 0 00 G + H cos4ψ H sin4ψ −sin τ sin2ψ

0 H sin4ψ G −H cos4ψ sin τ cos2ψ

0 sin τ sin2ψ −sin τ cos2ψ cos τ

I Q

U

V

(3.20)

where

G =12

(1 + cos τ ), H =12

(1 −cos τ ) (3.21)

If the direction of incident light makes a small angle i with the normal to the surface

of the retarder, and the plane of incidence makes an angle ω with the optic axis of



3.1.4:Transformation Equations for the Stokes parameters 47

crystal, the retardance at wavelength λ equals

τ ∼= 2π(ne −n0)(s/λ ) 1 −i2

2n0

cos2 ωn0 −

sin2 ωne

(3.22)

where s is the thickness of the retarder, while ne and n0 are the refractive indices

of its material for the extraordinary and ordinary rays, i.e., for the vibrations of the

electric vector of the light wave which are parallel and perpendicular to the optic

axis of the retarder, respectively.

From equations (3.19) and (3.20) we obtain the intensity of light transmitted through

a retarder with the optic axis at position angle ψ followed by an analyser with the

principal plane at position angle ϕ = 0 0 (upper signs) or ϕ = 90 0 (lower signs):

I =12

[I ±Q(G + H cos4ψ) ±UH sin4ψ V sin τ sin2ψ] (3.23)

For a quarter-wave plate τ = 90 0, G = H = 12 , and

I =12

(I ±12

Q ±12

Q cos4ψ ±12

U sin4ψ V sin2ψ) (3.24)

For a half-wave plate τ = 1800, G = 0 , H = 1 , and

I = 12

(I ±Q cos4ψ ±U sin4ψ) (3.25)

The transformation equation for two retarders in series is obtained by replacing

the square matrix in Equation (3.20) with a product of two such matrices for two

retarders. The intensity of light transmitted by two retarders of retardances τ 1

and τ 2 and optic axes at position angles ψ1 and ψ2, followed by an analyser with

the principal plane at position angle ϕ = 0 0(upper signs) or ϕ = 90 0 (lower signs)

(Ramachandran and Ramaseshan, 1961) is

I =12{I ±Q[G1G2 + H 1H 2 cos4(ψ1 −ψ2)

+ H 1G2 cos4ψ1 + G1H 2 cos4ψ2 −sin τ 1 sin τ 2 sin2ψ1 sin2ψ2]

± U [H 1H 2 sin4(ψ1 −ψ2) + H 1G2 sin4ψ1 + G1H 2 sin4ψ2

+ sin τ 1 sin τ 2 cos2ψ1 sin2ψ2] V [H 2 sin τ 1 sin(2ψ1 −4ψ2)

+ G2 sin τ 1 sin2ψ1 + cos τ 1 sin τ 2 sin2ψ2]} (3.26)



3.2.1:Photon Noise 48

In a special case of a quarter-wave plate followed by a half-wave plate and an analyser

at ϕ = 0 0 or 900, we have

I =1

2{I ±

1

2Q[cos 4(ψ

1 −ψ

2) + cos 4ψ

2]

±1

2U [sin 4(ψ

1 −ψ

2) + sin4 ψ

2]

V sin(2ψ1 −4ψ2)}, (3.27)

this combination offers interesting possibilities for the simultaneous measurement of

all Stokes parameters.

For two half-wave plates followed by an analyser, equation (3.26) takes a simple

form

I =1

2[I

±Q cos4(ψ1

−ψ2)

±U sin 4(ψ1

−ψ2)] (3.28)

the intensity of the transmitted light beam depends now on the angle between the

optic axes of two half-wave plates.

3.2 Error in polarisation measurementFor many astronomical objects, the observed polarisation is very small, making high

polarimetric accuracy essential. Polarimetric precision can be orders of magnitude

higher than photometric precision because the effects of atmospheric scintillation,

seeing and extinction can be eliminated. In this section various sources of error in

polarimetry will be discussed in details.

3.2.1 Photon Noise

The principal limitation of precision in astronomical polarimetry results from photon

statistics. If the polarimeter is not exceptionally bad, we may expect that wheneverthe error of percentage polarisation exceeds 0.2%, this error results from photon

statistics. Other sources of error become important only when better accuracy is

sought.

The mean error of each of the simultaneously determined normalised Stokes pa-

rameters Q/I and U/I , describing linear polarisation (Serkowski, 1962; Clarke &

Grainger, 1971) is

ε(Q/I ) = ε(U/I ) = 2/N, (3.29)



3.2.2:Atmospheric scintillation and Seeing 49

where N is the total number of photons counted. The only way to reduce the

error resulting from photon statistics is to count more photons. To make the most

efficient use of the light available, we should observe in a wide range of wavelengths

simultaneously, using many detectors. For each spectral range, the detectors of

highest quantum efficiency (Q. E.) in this range can be chosen. Different wavelengths

are separated either with dichroic lters , as was done successfully in a 10-channel

UBVRI polarimeter (Serkowski, 1974), or with a spectrometer coupled to a photon-

counting image tube.

Any device producing spectral dispersion changes the state of the polarisation of

light (Breckinridge, 1971; Poulsen, 1972). Therefore an analyser should be placed

in a xed orientation in front of the spectrometer or lters. This orientation should

be such that the light emerging from an analyser is polarised in a plane making

450 with the plane of incidence on a spectrometer grating or on dichroic lters; this

minimises undesirable polarisation effects in the instrument.

3.2.2 Atmospheric scintillation and Seeing

Since air is not birefringent, scintillation is same for both perpendicularly polarisedcomponents of light from an astronomical object. The ratio of intensities of two such

beams, emerging, eg., from a Wollaston prism, is free of the effects of atmospheric

scintillation and is not affected by the presence of thin clouds. Extinction by clouds

is nearly neutral in the visible region (Serkowski, 1970), and the accuracy of po-

larimetry through clouds is reduced only because of uctuations in sky background

and the smaller number of photons received. On the other hand, the atmospheric

seeing, i.e., the uctuations and spread in the direction from which we receive stel-lar light, affects the ratio of signals from two beams emerging from the Wollaston

prism. Because of the inhomogeneous sensitivity of detectors, atmospheric seeing

and imperfections in telescope guiding would spoil any hope of achieving high po-

larimetric accuracy in a system where an image of an astronomical object is formed

on photosensitive surfaces, unless the signals were modulated with high frequency.

The harmful effects of both atmospheric scintillation and seeing can be eliminated

by using at each spectral region two detectors for orthogonal polarisation and/or



3.2.3:Motion of Light Beam on Photocathode 50

by rapid modulation of the signal. The sinusoidal modulation with frequency f

diminishes the error of atmospheric origin in the amplitude of this modulation by a

factor ( f /f c)5/ 6, where f c is a cutoff frequency equal to

f c = V ⊥/ (πD ) (3.30)

Here D is the diameter of telescope and V ⊥ is the speed at which the wind drags

the shadow pattern past the telescope aperture; a typical value for V ⊥ is 3000cms − 1.

Assuming this value, we nd that the critical frequency of modulation, below which

photometric errors caused by atmospheric scintillation and seeing are not dimin-

ished, equals 20Hz for a telescope of 50cm diameter, and 2Hz for 500cm diameter.

3.2.3 Motion of Light Beam on Photocathode

As the distribution of sensitivity on photocathodes is usually very non-uniform,

accurate polarimetry with photomultipliers is possible only if the image of the tele-

scope mirror on a photocathode does not shift during the measurement by more than

about 0 .01% of its diameter. An optical element that is either rotated or inserted

into the light beam during the measurement should be plane parallel with an accu-racy of a few seconds of arc to avoid shifting an image on the photocathode. The

requirements for plane parallelism are relaxed if an image of the telescope mirror is

formed on the rotating optical element which is then re-imaged on the photocathode

(Serkowski, 1974).

The problems caused by the inhomogeneous sensitivity of a photocathode become

particularly serious when, instead of an image of telesope mirror, an image of an

astronomical object or of its spectrum is formed on the photocathode of a photon-counting image tube. Such an image is subject to shifts caused by inaccurate tele-

scope guiding or bad seeing. Achieving high polarimetric accuracy is then possible

only with a rapid modulation of the signal by a rotating retarder in front of a sta-

tionary analyser. This retarder should be placed as close as possible to the telescope

focal plane to relax the requirements for its plane parallelism. A rotating half-wave

plate has a convenient feature of modulating the polarisation at a frequency four

times higher than that of a mechanical rotation. This again relaxes considerably



3.2.5:Variable Sky Background 51

the requirements for plane parallelism of the retarder; nevertheless, for precise po-

larimetry in most cases a half-wave plate should be plane parallel to an accuracy of

at least l arc minute.

3.2.4 Unnecessary Reections from Optical Components

In a polarimeter, care should be taken to eliminate the unnecessarily reected light

from optical components. Particularly harmful if the light is doubly reected from

surfaces of a Wollaston prism. The amount of reected light that reaches the detec-

tors usually depends strongly on the position of the image of the observed object in

the focal plane diaphragm. This makes the resulting systematic errors particularly

difficult to eliminate.

One way to prevent the doubly reected light from reaching the detectors is to tilt

Wollaston prism, and all other stationary optical components with at surfaces,

with respect to the axis of the polarimeter.

3.2.5 Variable Sky Background

Polarisation of the background sky can be eliminated by observing a star centeredin the middle one of three identical focal plane diaphragms. The light from the

diaphragms, after going through a Wollaston prism, should form images of the star

close to two Fabry lenses placed in front of two photomultipliers. The centers of

three focal plane diaphragms should lie on a straight line spaced so that an ordinary

image of the central diaphragm on one of the Fabry lens is superimposed upon an

extraordinary image of the left diaphragm; in such a pair of superimposed images;

the light of the background sky becomes unpolarised. Similarly on the other Fabrylens an extraordinary image of the central diaphragm is superimposed upon an

ordinary image of the right diaphragm.

An advantage of this method of eliminating the polarisation of the background

sky is that the background needs to be measured much less frequently than would

otherwise be necessary. We need now only to know the brightness of background

sky, not the polarisation. For faint objects, for which the signal is not more than

twice as strong as the signal from sky background, we should be able to obtain the



3.2.7:Zero Point of Position Angles 52

desired polarimetric accuracy in half the time by using three diaphragms rather than

by using the conventional single diaphragm. Thus variable sky background can be

remedied by rapid switching between object & sky, and cancelling polarisation of

sky background by superimposing perpendicularly polarised images of the sky.

3.2.6 Effective Wavelengths

An important source of errors between the observations made with different po-

larimeters is the inaccurate knowledge of the effective wavelengths of the spectral

regions used. Such errors could be easily avoided because every polarimeter has an

inherent ability of measuring the effective wavelengths with high accuracy. All that

is needed is to measure the polarisation of the objects studied with a polariser and

a suitable retarder inserted in front of a polarimeter.

For wide-band spectral regions between 0.3 and 1 .1µm, a quartz retarder, which is

a quarter-wave plate at 0 .45µm, is most suitable. If an optic axis of this retarder

makes 450 with the principal plane of the polariser, having good ultraviolet trans-

mittance, the degree of linear polarisation for light emerging from the retarder is

approximately proportional to the inverse of wavelength, with the position angleipping by 900 at 0.45µm. Measuring polarisation with a precision of ±0.1% gives

an effective wavelength accurate to ±3A in the blue spectral region. Similarly, a

thick wide-angle retarder can be used for calibrating a spectrum scanner with an

accuracy of ±0.01% or better (Serkowski, 1972), which makes possible the accurate

measurements of radial velocities with wide open (∼1A) entrance and exit slits of

the scanner.

3.2.7 Zero Point of Position Angles

A very accurate calibration of position angles in an equatorial coordinate system can

be obtained by replacing the diagonal mirror which reects the light to the viewing

eyepiece in the polarimeter, by a plane parallel stress-free glass plate. The telescope,

with clock drive stopped, is pointed in such a direction that a spirit level put on

this glass plate indicates its exact horizontal orientation. The position angle of the

plane of incidence of the telescope axis on a glass plate can now be calculated from



3.3.1:Efficiency of the Polarimeter 53

the readings of the declination and hour angle circles. This is compared with the

position angle of polarisation measured for any unpolarised standard star through

the glass plate remaining tilted to the telescope’s optic axis at the same angle at

about 45 0. Since the linear polarisation introduced by such a tilted plate amounts to

about 9%, the position angles can be easily measured with an accuracy on the order

of a minute of arc. To eliminate the effects of the deviations of the glass plate from

the plane parallelism and its strain birefringence, the calibration should be repeated

at different orientations of the glass plate.

3.3 Different kinds of polarimetersPolarisation measurements on comets provide a very good tool to study the cometary

dust and other properties. Different techniques of polarisation measurements on

comets have been recently outlined by Sen (2001). In this section, a brief study of

different polarimeters are discussed.

3.3.1 Efficiency of the Polarimeter

Let the light of an astronomical object incident on a polarimeter be described by

the Stokes parameters I, Q, U and V. Denoting the signals (photon counts) from

two beams emerging from a beam-splitting analyser (e. g., a Wollaston prism) by

I 1 and I 2, all the information on the state of polarisation of incident light should be

contained in the difference I 1 −I 2. This difference can be represented by the form:

I 1 −I 2 = Qf Q (t) + Uf U (t) + V f V (t) + c(I,Q,U,V ), (3.31)

where the mean values of the functions f Q , f U and f V , averaged over time t duringthe measurement are equal to zero, and the function c is independent of the time.

The values of these four functions can be found from equations (3.19) and (3.23)

through (3.27) . Equation (3.31) holds also for a one channel polarimeter, in which

case I 2 = 0.

The efficiencies of a polarimeter for linear and circular polarisation are dened as

E lin = < f 2Q (t) + f 2U (t) >, (3.32)

E cir = < f 2V (t) >, (3.33)



3.3.2:Polarimeters without Rapid Modulation Of the Signal 54

where angular brackets denote the averaging over the duration of measurement last-

ing a unit of time. The efficiencies E lin and E cir are inversely proportional to the

amount of time needed for obtaining a given polarimetric precision for the incident

light of intensity I ; they are equal to 1 for a perfect polarimeter. The meaning of

equation (3.31) may be more easily understood when both sides of this equation are

divided by the intensity I of incident light and the equation takes the form:

(I 1/I 2) −1(I 1/I 2) + 1

T =QI

f Q (t) +U I

f U (t) +V I

f V (t) + c (QI

+U I

+V I

), (3.34)

where T is a transmittance of the polarimeter for unpolarised light.

3.3.2 Polarimeters without Rapid Modulation Of the Signal

The simplest type of polarimeter is a polaroid rotated in discrete steps in front of a

detector. The work by Sen et al. (1990) can be cited as an example for the efficient

use of such a polarimeter for comet work. Since only the light linearly polarised

in the principal plane of a polaroid is transmitted , the efficiency E lin , calculated

from equations (3.19) and (3.32), can not exceed 12 . A depolariser must be placed

between the polaroid and the detector to eliminate the dependence of sensitivity onthe plane of polarisation, occuring for most detectors. This limits the applications

of such a polarimeter to wide spectral regions because, constructing monochromatic

depolarizers (Billings, 1951) is difficult.

The most widely used type of polarimeter without rapid modulation of the signal

is called Wollaston polarimeter . The efficiency of the Wollaston polarimeter, as

results from equations (3.19), (3.32) and (3.34), would equal E lin = 1 if there were

no need to use the depolariser. Actually, instead of equation (3.34), we have for theWollaston polarimeter

(I 1I 2

.I 2d

I 1d −1)/ (I 1I 2

.I 2d

I 1d+ 1) =

QI

cos2ϕ +U I

sin2ϕ, (3.35)

where subscript d denotes the measurement with depolariser and ϕ is the position

angle of the polarimeter. If each of the ratios I 1/I 2 and I 1d/I 2d is measured with a

mean error ε, the mean error of I 1I 1d/I 2I 2d equals 21/ 2ε. If a depolariser were not

used, twice as much as of the observing time would be spent on observing I 1/I 2,



References 55

and its mean error would decrease to 2 − 1/ 2ε. Therefore, in unit observing time, the

left side of equation (3.35) is measured with a mean error twice as large as that for

the left side of equation (3.34); hence, when a depolariser is used, the efficiency of

the Wollaston polarimeter equals E lin = 14 . Obtaining any desired precision with

this Wollaston polarimeter takes four times as much observing time as with an ideal

polarimeter.

The simplest method of increasing the efficiency of a Wollaston polarimeter to

E lin ∼= 1 is to replace the measurements with and without a depolariser by the

measurements at two orientations of a Wollaston prism relative to the polarimeter,

differing by 1800 . The Wollaston prism must be, in this case, relatively thin and

must consist of three components (Soref and McMahon, 1966) so that the shift of

the images of the telescope mirror on the photocathodes caused by rotation of the

Wollaston prism is negligibly small. An image of the telescope mirror should be

formed on the Wollaston prism to diminish this shift and to make it independent

of small deviations of the angle of rotation of the Wollaston prism for 180 0. The

Wollaston prism must be followed by a thick retarder, with an optic axis at 45 0 to

the principal plane of the Wollaston prism, to act as a depolariser. The need for

this depolariser and the necessity for rotating the entire instrument are the main

disadvantages of this type of polarimeter.

3.3.3 Polarimeters with Rapid Modulation Of the Signal

Rapid modulation of the signal is the only way to eliminate the polarimetric errors

caused by atmospheric seeing and by inaccurate telescope guiding. These are the

main sources of error for bright stars observed without rapid modulation. A modu-lation at very high frequency can be obtained by using a Pockels cell or piezooptical

modulator. In the Pockels cell, a crystal, KDP for example, changes its birefrin-

gence in phase with a rapidly changing high voltage applied to its surface. In

the piezooptical modulator, the stress birefringence is produced in a transparent



References 56

isotropic material by acoustic vibrations.

ReferencesBillings B. H., 1951, J. Opt. Soc. Amer. , 41 , 966.

Breckinridge J. B., 1971, Applied Optics, 10 , 286.

Chandrasekhar S., 1950. In Radiative transfer . Oxford Univ. Press, London.

Clarke D. & Grainger J. F., 1971. In Polarized light and optical measurement ,

Oxford: Pergamon.

Poulsen O., 1972, Applied Optics, 11 , 1876.

Ramachandran G. N. & Ramaseshan S., 1961. In Handbuch der Physik . Ed. S.

Flugge, vol 25 , 1, Spinger Verlag, Berlin.

Sen A.K,, Joshi U.C., Deshpande M.R., & Debiprasad C. 1990, ICARUS , 86 , 248.

Sen A.K,, 2001, Small Telescope Astronomy on Global Scales ASP Conf. Series ,

edt W P Chen, C. Lemme, & B. Paczynski, 86 , 275.

Serkowski K., 1962, Adv. Astron. Astroph. , 1, 289.

Serkowski K., 1970, Publ. Astron. Soc. Pac. , 82 , 908.

Serkowski K., 1972, Publ. Astron. Soc. Pac. , 84 , 649.

Serkowski K., 1974. In Planets, stars and nebulae studied through photopolarimetry .

Ed. T. Gehrels, Univ. of Arizona Press.

Soref R. A. & MacMahon, 1966, Applied Optics, 5, 425.

Stokes G. C., 1852, Trans. Cambr. Phil. Soc. , 9, 399.

van de Hulst H. C., 1957. In Light Scattering by Small Particles . Wiley, New York.



Chapter 4

POLARIMETRIC DATA

ANALYSIS USING MIE THEORY

This chapter begins with the introduction of different light scattering theories which

are used for the study of cometary grains. Then Mie scattering theory for spherical

particles is discussed. The in situ dust measurements of comet Halley are also

discussed. Finally, the polarimetric data of comet Halley is analysed using Mie Theory.

4.1 Light Scattering TheoryThe theory of scattering of light by small particles is basic to the study of cometary

grains. Actually, this theory determines the distribution of intensity of the scattered

radiation and the polarisation as a function of the scattering angle. Also the cross

sections for the absorption and scattering processes, which determine the albedo

of the particle, can be computed from scattering theory. The efficiency factor for

the radiation pressure and other quantities are also of interest. All these quantities

depend upon the the shape, structure and composition of the grain. The theo-

ries of scattering have been developed for well-dened particle shapes like spheres,

concentric spheres, cylinders, spheroids and so on.

The following scattering theories are widely used for the analysis of cometary grains:

57




4.1.1:Light scattering by spherical particles : Mie Theory 58

1. Mie theory

2. T-matrix Theory

3. Discrete Dipole Approximation (DDA) etc.In this chapter, Mie Theory is discussed. Using this theory, polarimetric data of

comet Halley is analysed. In Chapter 5 , the polarimetric data of other comets are

studied using Mie Theory. The T-matrix Theory is discussed in Chapter 6 and the

polarimetric data of comet Levy 1990XX at λ = 0.485µm is analysed using this

theory.

4.1.1 Light scattering by spherical particles : Mie Theory

Mie (1908) proposed the theory of scattering of plane electromagnetic waves by a

homogeneous, isotropic and smooth sphere of arbitrary size and refractive index.

The theory of scattering by spherical particles of homogeneous composition involves

the solution of Maxwell’s equations with appropriate boundary conditions on the

sphere.

The scattering properties of a particle depend upon the following quantities:

(i) The property of the medium, usually specied by the complex refractive index,

m = n −ik , where n and k are the refractive and absorptive indices respectively,

(ii ) the wavelength of the incident solar radiation ( λ),

(iii ) the size of the particle ( a) and

(iv) scattering angle ( θ).

When radiation interacts with the particle, part of the radiation is absorbed and

part of it is scattered. Thus, the total amount of radiation lost from the incidentbeam (extinction) is the sum total of the absorbed and scattered components. These

are generally expressed in terms of the dimensionless efficiency factors Qsca and Qabs

for the scattering and absorption components.

The efficiency factors for the total extinction is given by

Qext = Qsca + Qabs (4.1)

If C sca , C abs and C ext denote the corresponding cross sections, then

C sca = πa 2.Qsca (4.2)



4.1.1:Light scattering by spherical particles : Mie Theory 59

C abs = πa 2.Qabs (4.3)

C ext = πa 2.Qext (4.4)

From the scattering theory, the efficiency factors Qsca

and Qabs

are given by

Qsca =2x2

∞

n =1(2n + 1) {|an |2 + |bn |2} (4.5)

Qext =2x2

∞

n =1(2n + 1) {Re(an + bn )} (4.6)

where, x = size parameter = 2πaλ , Re represents the real part and an ,bn are Mie

Coefficients.

The scattering coefficients an and bn are given by

an =ψn (mx ).ψn (x) −mψn (mx ).ψn (x)ψn (mx ).ζ n (x) −mψn (mx ).ζ n (x)

(4.7)

bn =mψn (mx ).ψn (x) −ψn (mx ).ψn (x)mψn (mx ).ζ n (x) −ψn (mx ).ζ n (x)

(4.8)

ψn and ζ n are the modied Bessel functions known as the Riccati - Bessel functions.

Riccati - Bessel functions can be expressed in terms of Bessel function, J, as follows:

ψn (y) = (πy

2)1/ 2J n +1 / 2(y) (4.9)

and

ζ n (y) = (πy2

)1/ 2[J n +1 / 2(y) + i(−1)n J − n − 1/ 2(y)] (4.10)

where y represents either mx or x. The third Riccati - Bessel function can be dened

as

χ n (y) = ( −1)n (πy2

)1/ 2J − n − 1/ 2(y) (4.11)

The functions ψn (y) and χ n (y) are connected through the identity:

ζ n (y) = ψn (y) + iχ n (y) (4.12)

The albedo of the particle is dened as

γ =Qsca

Qext(4.13)

If I 0 is the original intensity impinging on the grain, the intensity of the light scat-

tered into unit solid angle for the scattering angle θ dened w.r.t. the incident beam

is given by F (θ)I 0, where F (θ) denotes the phase function.



4.2:The in situ dust measurements of Halley 60

The scattering phase function is related to the complex scattering amplitudes S 1(θ)

and S 2(θ) as

F (θ) =1

2k2 [|S 1(θ)|2 + |S 2(θ)|2] = I ⊥ + I (4.14)

The quantity I ⊥ and I are the components of intensity in the direction perpendicular

and parallel to the scattering plane. The scattering plane contains the incident

radiation and the direction of the scattered wave.

The expressions for S 1(θ) and S 2(θ) are given in terms of the scattered coefficients

an and bn as

S 1(θ) =∞

n =1

(2n + 1)n(n + 1)

[an πn (cosθ) + bn τ n (cosθ)] (4.15)

S 2(θ) = ∞

n =1

(2n + 1)n(n + 1)

[bn πn (cosθ) + an τ n (cosθ)] (4.16)

where,

πn (cosθ) =1

sinθP 1n (cosθ) (4.17)

and

τ n (cosθ) =ddθ

P 1n (cosθ) (4.18)

Here P n s are the Legendre polynomials.

The degree of polarisation of the scattered beam is given by

p =I ⊥−I I ⊥ + I

(4.19)

The value of p varies from 0 to 1. The sign of p could be positive or negative.

Positive and negative signs imply that the scattered light is polarised perpendicular

or parallel to the scattering plane respectively. If θ = 0 0 or 1800, value of p is equal

to zero as I ⊥ = I .

In addition to linear polarisation, circular polarisation also may be seen in certain

cases. The circular polarisation arises if the refractive indices are different for the

two states of polarisation.

4.2 The in situ dust measurements of HalleyDuring the last apparition of comet Halley, the various space probes on board Vega

I, Vega II and Giotto carried out measurements to determine the number density




of particles of given masses. However, the exact determination of the particle size

distribution function from the above data needs a number of assumptions to be

made. Hence, it is very crucial to analyse the ground based observations (related to

dust properties), with reference to the in situ observations, to check the consistency

of both set of results. In this context, amongst various other types of measurements,

the polarimetry of comets in the continuum plays an important role in the study of

cometary dust properties.

Based on SP-2 experiment on-board Vega space-craft, Mazets et al. (1986) had

suggested a set of power laws ( with separate indices for different mass ranges )

for particle mass distribution over the range 10 − 16g to 10− 7g. Subsequently, Mukai

et al. (1987) used these distribution functions to explain their optical polarimetric

observations of Halley. Assuming grain bulk density to be 1 g cm− 3, they arrived at

the following size distribution functions:

N (s) ∼s− 2, s < 0.62µm (4.20)

N (s) ∼s− 2.75 , 0.62µm < s < 6.2µm (4.21)

N (s) ∼s− 3.4, s > 6.2µm (4.22)

Sen et al. (1991a) followed the same approach in their analysis of the polarimetric

data of Halley. Lamy et al. (1987) combined the in-situ dust measurements from the

Vega-I, Vega-II and Giotto and modelled the dust mass distribution, as a polynomial

of the form:

log N c(m) =3

i=0a i(log m)i (4.23)

where, N c(m) is the cumulative number density of dust particles with mass > m

and the coefficients (a i) are determined by the least square method.

These authors further derived the differential spatial density N(s) as a function of

grain radius (s), given by

N (s) = −3N c

s

3

i=1ia i(log m)i− 1 (4.24)

The size distribution function derived by Mukai et al. (1987) on the basis of the

work reported by Mazets et al. (1986) has three discrete size ranges and the size

distribution function changes its value abruptly over the three ranges due to the




presence of three distinct values of power law index. On the contrary the size

distribution function as in equation (4.24) ( from Lamy et al.1987) has a smooth

behaviour.

The dust distribution function derived by Mazets et al. (1986) is actually based

on only Vega II results, while the work of Lamy et al. (1987) is based on three

space-craft results. Since in this work the plan is to analyse polarimetric data of

various comets, one proceeds with the dust distribution function suggested by Lamy

et al. (1987). These authors have listed the values of bulk density and ( n, k ) for

different grain materials and have justied the value 2.2 g cm− 3 for bulk density in

most cases corresponding to materials like chondrite, magnetite or silicates. Present

work uses this value of bulk density to construct Table 4.1 , which gives values of

log (s) and corresponding log N(s). The plot of the data and the best-t second

degree polynomial curve to it (done in the present work) are shown in Figure 4.1 .

The second degree polynomial used has the form,

log N (s) = a(log s)2 + b(log s) + c (4.25)

where, a = −0.2593, b = −4.422 c = −15.06. The polynomial seems to t the dataof Lamy et al. (1987) quite well, as can be seen in Figure 4.1 . This grain model is

used in the subsequent part of the work here. However, one notes that the grain size

distributions used by Mukai et al. (1987)(equations (4.20-22)), or the one derived

from Lamy et. al. (1987)( equation 4.25) are basically the ones obtained after the

last apparition of comet Halley in 1985-86 and were invoked in explaining mostly

the polarisation properties of comets. In the post-Halley era, infra-red observations

of different comets have given many new diagnostics to understand grain properties.In a recent imaging polarimetric work on comet Hale Bopp, a very useful discussion

has been made by Hadamcik and Levasseur-Regourd (2003b) on the polarimetric

results with reference to the results obtained by other diagnostics viz., albedo derived

from NIR observations, 10 µm silicate emission feature, emission in sub-millimeter

domain, colour temperature and bright structure of grains. A different grain size

distribution has been used in the interpretation of NIR




.




-8

-6

-4

-2

0

2

4

-7 -6 -5 -4 -3 -2

L o g

N ( s )

Log(s)

-0.2593*(Log(s)**2)-4.4223*Log(s)-15.06

Figure 4.1: Log of grain radius ( s in cm) against the log of differential spatial density ( N (s) in cm− 4) as obtained from Lamy et al. (1987) for comet Halley derived through space-craft experiments (Table 4.1). The dotted curve represents the best-t polynomial equation as derived in the present work.




Table 4.1: The log of grain radius ( s) and log of differential spatial density

(N (s)) as derived from Lamy et al. (1987).

log(s) log N (s)

(s in cm) (N (s) in cm− 4)

-7.0 3.50

-6.5 2.67

-6.0 1.90

-5.5 1.18

-5.0 0.44-4.5 -0.39

-4.0 -1.37

-3.5 -2.53

-3.0 -3.91

-2.5 -5.57

-2.0 -7.54



4.3:Polarimetric data of Halley and grain characteristics 66

emission from grains (Harker et al.2002, Hanner and Hayward 2003).

A discussion on the grain model of Lamy et al.(1987) (refer equation 4.25) in the

context of recent results obtained from other diagnostics is expected to lead to a

renement in the grain size distribution used in the study of comets. However, it

requires a very detail analysis. So far no unied grain model has been suggested

to take care of both types of observations. Apparently, failure in xing a unied

grain model for both types of observations may be due to the fact that grains which

are powerful polarisers may not be good emitters in IR. For example by tting

the thermal grain model to NIR spectra of comet Hale Bopp without including a

scattered light component, Hayward et al. (2000) derived a smaller peak grain size

much out side 1σ uncertainty.

Therefore, without going further into this analysis in an attempt to nd a unied

grain model, one chooses here the grain model which has been successfully used

earlier to explain cometary polarisation (Mukai et al., 1987; Krishnaswamy and

Shah, 1988; Sen et al., 1991a ). This amounts to the selection of equation (4.25) as

a slightly modied grain model for the present work.

The detectors on-board the Vega and Giotto spacecrafts had sensitivities as low as

10− 16 gm, and it was observed that the particle number density continued to increase

till the lowest end of detection limit was reached (Mazet et al. 1987). Assuming

spherical particles of density 1 or 2.2 gm per cc, one derives a lower limit of particle

radius as 0.01µm. However, as 0.001−20.0µm size range has been already used by

Sen et al. (1991a) and Krishnaswamy and Shah (1988) for the analysis of polarimetry

results, one continues using here the same size range; so that very small particles

are not left out. This has also been done with a view to compare the present studies

with previous similar polarimetric studies. The selection of 0 .001µm or 0.01µm as

the lower limit of size range changes the calculated value of percent polarisation only

at the fourth place after the decimal. The selection of lower limit as 0 .001µm or

0.01µm in no way changes the conclusions arrived at, in this work. Also it is to be

noted that though, the lower limit of grain size distribution has xed at 0 .001µm,

but one may as well assume the lower limit to be 0 .01µm, if one wants to compare

with other similar work.




4.3 Polarimetric data of Halley and grain charac-

teristics

During the last apparition of comet Halley, IHW was coordinating the ground basedobservations and suggested a set of eight narrow band interference lters for po-

larimetry and photometry, out of which three correspond to continuum.

Based on the grain model of Mazets et al. (1987) and Mie Theory, Mukai et al.

(1987) found out a set of three complex refractive indices (n,k) at three IHW con-

tinuum wavelengths which best match their observations.

Again Sen et al. (1991a) combined their polarimetric observations with those of

other investigators and minimised the sum of squares of differences between observedpolarisation and calculated polarisation values to estimate (n,k) values and found,

refractive indices to be only slightly different from those of Mukai et al. (1987).

In the present study, equation (4.25)is used for grain distribution as against equa-

tions (4.20-22) and a value of 2.2 g cm− 3 is used for the bulk density of grains as

justied by Lamy et al. (1987). One also chooses a grain size range 0.001µ to 20µm,

as discussed earlier. Using the Mie theory, one may determine the best t values of

(n,k) at which the sum of squares of differences between the calculated and observed

values of polarisation becomes minimum. These values are listed in Table-4.2 .

Figures (4.2),(4.3) and (4.4) , show curves that give the calculated values of polar-

isation as against the observed polarisation values reported by various authors, at

wavelengths λ = 0 .365, 0.484, 0.684 µm respectively.




Table 4.2: The (n, k ) values obtained by previous authors and in thepresent work, for comet Halley at different wavelengths.

λ n k Authors

0.365 µm 1.392 0.024 Mukai et al. (1987)

1.387 0.032 Sen et al. (1991a)

1.403 0.024 Present work

0.484 µm 1.387 0.031 Mukai et al. (1987)

1.375 0.040 Sen et al. (1991a)


0.620 µm 1.385 0.035 Mukai et al. (1987)

0.684 µm 1.374 0.052 Sen et al. (1991a)





-10

-5

0

5

10

15

20

25

30

110 120 130 140 150 160 170 180

P o

l a r i z a t i o n

( i n % )

Scattering angle (in degrees)

Halley at 0.365 micron

Figure 4.2: The observed polarisation values of comet P/Halley at λ = 0 .365µm.The dotted curve represents the calculated values for Mie type scattering with

(n, k ) = (1 .403, 0.024).




-10

-5

0

5

10

15

20

25

110 120 130 140 150 160 170 180

P o

l a r i z a t i o n

( i n % )




(n, k ) = (1 .390, 0.026).




-10

-5

0

5

10

15

20

25

30

110 120 130 140 150 160 170 180

P o

l a r i z a t i o n

( i n % )




(n, k ) = (1 .386, 0.038).



References 72

ReferencesHadamcik E., and Levasseur-Regourd A.C., 2003b, A&A, 403 , 757.

Hanner M.S. and Hayward T. L. 2003, Icarus , 161 , 164.

Harker D.E., Wooden D.H.,Woodward C.E., Lisse C. M., 2002, ApJ , 580 , 579.


Krishnaswamy K.S. and Shah G.A., 1988, MNRAS 233 , 573.


Mie G., 1908, Ann. Physik , 25 , 377.






242 , 496.



Chapter 5

ON THE VARIATION OF

POLARIMETRIC PROPERTIES

OF DIFFERENT COMETS

In this chapter polarimetric observations on several comets are discussed. Then

observed variation in polarisation properties between different comets is discussed.

Also a model is proposed to explain this observed variation, in terms of grain aging

of comets by solar radiation.

5.1 Observed polarimetric variation among cometsThe measurement of polarisation of the scattered radiation from comets, over var-

ious phase angles and wavelengths, provides an excellent tool to study cometary

dust properties. The polarisation is caused mainly by scattering of solar radiation

by cometary dust grains. Analysis of these polarisation data reveals the physical

properties of the cometary grains, which include size distribution, shape and complex

refractive index. As discussed in Chapter 4 , the in situ space-craft measurement of

Halley gave the rst direct evidence of grain mass distribution ( Mazets et al. 1986,

Lamy et al (1987). The dust size distribution functions N (s) (with bulk density

of dust = 2.2 g per cc) for comet Halley has been already derived in Chapter 4

following Lamy et al. (1987).

73




5.1:Observed polarimetric variation among comets 74

However, there is a modied form of power law dust size distribution differing sub-

stantially in the abundance of larger particles, which has been successfully used

to explain the observed Spectral Energy Distribution (SED) in the thermal (IR)

emission from cometary particles (Harker et al. 2002, Hanner & Hayward 2003).

Since the last apparition of Halley’s comet, many other comets were observed in

polarimetry and the analysis of these data clearly shows that the dependence of

polarisation on phase angle and wavelength varies widely from comet to comet (

Chernova et. al. 1993, Levasseur-Regourd et al. 1996, Hadamcik and Levasseur-

Regourd 2003a etc.).

Comet Austin was observed polarimetrically by Sen et al. (1991b) and the authors

compared the data with those of Halley. The two comets exhibited different types

of phase angle dependence at the same wavelength. Using Mie Theory the authors

argued that the observed differences can be explained if at least one of the two grain

properties viz. size distribution and composition differs from one comet to other.

Following the suggestion of Delsemme (1987) that grain composition is less likely

to differ between any two comets, Sen et al. (1991b) also showed that a better

t of the data to the predictions of Mie theory indeed results if variations in size

distribution alone are considered to be present. The sizes are expected to increase

with the dynamical age of comets, due to sintering (among other processes) by solar

radiation (Delsemme 1987). Halley being a dynamically older comet than Ausin one

may nd it reasonable to expect that the grains of Austin to be ner than that of

Halley.

The increase in size with age can have reasons other than sintering. The smaller

grains are preferentially pushed away by solar radiation pressure, leaving the larger

ones in orbit around the nucleus of the comet. It has also been observed that

the composition of the nucleus does not seem to differ from one comet to another

(A’Hearn 1999). Now since the nucleus is the sole source of grains in comets, one

may expect that the composition of grains does not differ from one comet to other.

Therefore, if required one may vary the size distribution to t the observed data to

model.

Harker et al (2002) suggested a mechanism in which the action of solar radiation



5.2:Observed relative abundance of coarser grains in different comets 75

increases the size of the nuclear pore, through which grains are released. A larger

pore size (caused due to nearness to the Sun) allows larger grains to be released

from the nucleus. Thus the action of solar radiation on the surface of the nucleus

alters the grain size distribution towards larger sizes. Also a good model t of

the observed IR data of Comets Hale-Bopp and Mueller(C/1993 A1) was obtained

by the authors with a change in size distribution alone, rather than a change in

composition (mineralogy). Harker et al.(2002) had also suggested that different grain

compositions between comets are less likely, but a different grain size distribution

could play an important role to explain differences in IR emission from different

comets.

With this background, in the present work it is tried to understand whether the

observed differences in polarisation behaviour of different comets can be understood

in terms of the variation in grain size distribution.

Levasseur-Regourd et al. (1996), studied a polarimetric data base of 22 comets and

from the nature of the phase angle dependence, concluded that there is a clear ev-

idence for two classes of comets. More recently Hadamcik and Levasseur-Regourd

(2003a) compared the imaging polarimetry of seven different comets and suggested

that Hale Bopp itself represents a new third class, marked by unusually high polar-

isation. The behaviour of polarisation and polarimetric colours of different regions

of several comets were discussed taking into account different grain properties.

In the present work, the post Halley polarimetric observations of various comets are

used and their behaviour are analysed with the following objectives:

(i) The assumption made by Sen et al.(1991b) and the idea put forth by Delsemme

(1987) are extended to all other comets, so that one can characterise each comet

by an individual grain size distribution, with xed complex refractive index for all

comets.

(ii ) The relative abundance of coarser grains in a comet (as derived from the grain

size distribution) is estimated and explored if such relative abundances are in anyway

related to its dynamical age.




5.2 Observed relative abundance of coarser grains

in different comets

Polarimetry has always been considered a powerful tool in the study cometary dustproperties (Sen 2001). In the present work, data is compiled on the polarisation

observations that were made through IHW continuum lters and published in var-

ious journals. No claim to completeness is suggested here, but whatever data was

available, has been included. When including data, a selection criteria is imposed

that the number of data points should be at least ve, since the number of tting

parameters is of the same order. Table-5.1 lists the names of the comets that were

considered in this work and the corresponding references for the source of data. Inthe same table, one can also note the two orbital elements q ( perihelion distance in

A.U.) and T (time period in years), which will be used in the subsequent section.

The polarisation data used here are reported at various phase angles, and if one

assumes Mie theory, one can t the observed data to the expected curve, with ( n, k )

and the co-efficient a,b,c (of equation (4.25)) as the free parameters. From equation

(4.25) one can show the calculated polarisation value will not depend upon c, as it

can not inuence the relative abundances of different sizes. Therefore, as has been

already discussed in Section 5.1 , one can keep the composition ( n, k ) xed and vary

the size distribution ( a, b) alone.

Thus, if one can narrow down the search procedure by xing the ( n, k ) values xed

to that of Halley and try tting the parameters a, b of equation (4.25), one can

obtain individual grain size distribution functions for different comets by specifying

a, b. It is clearly seen from equation (4.25) that the value of d log( N (s))d log s is proportional

to the relative abundances of coarser grains. Equation (4.25) further suggests that

d log(N (s))d log s

= 2 a log s + b, (5.1)

which can be xed at a denite value of s (say s = 10 − 7cm or 0.001µm) for purposes

of comparison between various comets. This can be done by adjusting the value of

c among various comets – a change in c will not change the calculated value of

polarisation.




Table 5.1: The ‘relative abundance of coarser grains’ ( g) for different

comets along with their orbital parameters

Comet Scatt. angle No. of q T Estimated Source of

range (0 ) data points values of a, b, g pol. data

Austin 72 - 165 6 0.350 ∞ -0.283, -5.24, -1.28 Ref.7

(1990 V) (λ =485 nm ) (Ref.1) Ref.8

71 - 117 4

(λ =684 nm )

Bradeld 124 - 147 7 0.871 ∞ -0.169, -4.57, -2.20 Ref.9

(1987 XIII) ( λ =485 nm ) (Ref.2) Ref.7Faye 154 - 157 4 1.59 7.34 -0.184, -4.35, -1.77 Ref.7

(1991n) ( λ =485 nm ) (Ref.3)

Hale-Bopp 133 - 163 29 0.914 4000 -0.248, -4.82, -1.35 Ref.10

(C/1995 O1) ( λ =485 nm ) (Ref.4) Ref.11

133 - 177 57

(λ =684 nm )

Halley 114 - 178 43 0.587 76.1 -0.259, -4.42, -0.79 Ref.12

(1986 III) (λ =365 nm ) (Ref.4) Ref.13

114 - 178 71 Ref.14

(λ =485 nm ) Ref.15

114 - 162 25 Ref.7

(λ =684 nm )

Hyakutake 69 - 143 11 0.230 ∞ -0.257, -4.50, -0.91 Ref.16

(λ =485 nm ) (Ref.5) Ref.17

(1996 B2) 69 - 143 13

(λ =684 nm )

Kopff 143 - 162 6 1.59 6.46 +0.174, -1.23, -3.67 Ref.7

(1983 XIII) ( λ =485 nm ) (Ref.6)

Levy 122 - 161 16 0.94 ∞ -0.049, -3.17, -2.48 Ref.7

(1990 XX) (λ =485 nm ) (Ref.4)

Ref. (1) IAUC 4972/MPC 16001, (2) IAUC 4442, (3) MPC 27081, (4) Marsden and Williams,

1995, (5) IAUC 6329, (6) MPC 34423, (7) Chernova et al., 1993, (8) Sen et al., 1991b, (9) Kikuchi

et al., 1989, (10) Ganesh et al., 1998, (11) Manset & Bastien, 2000, (12) Bastien et al., 1986, (13)

Kikuchi et al., 1987, (14) Le Borgne et al., 1987, (15) Sen et al., 1991a, (16) Joshi et al., 1997, (17)

Kiselev & Velichko, 1998



5.3:A model to explain the variation 78

From equation (4.25),

N (s) = 10 a(log s)2 + b(log s)+ c (5.2)

It can be written as:

dN (s)ds

=dN (s)d log s

d log sds

= N (s)(2a log s + b)1s

loge 10

Therefore,dN (s)

ds=

N (s)s

(d log N (s)

d log s)loge 10

Now if the N (s) values of different comets at a xed value of s are normalised, say

at s = 10 − 7cm, one may write

d log(N (s))d log s

= ( constant )∗d(N (s))

ds, (5.3)

This value of d log( N (s))d log s as expressed by equation (5.1) can be considered as a ‘relative

abundance of coarser grain’ index which is denoted by g. Thus, g = −14a + b. It

is to be noted that g can be considered as the gradient of tangent drawn to the

grain distribution curve N (s) at the point s = 10 − 7cm. The best t values of a

and b required to minimise the sum of squares of differences between the observed

and calculated values of polarisation are determined. The values of g so calculated

for different comets are listed in Table-5.1 . It can be seen from Table-5.1 , thatd log( N (s))

d log s or g value for Halley is -0.79, and that of Austin is -1.28, at s = 0 .001µm.

This suggests that comet Halley contains a relatively larger number of coarser grains

as compared to Austin.

The infrared spectra of comet Austin, however, suggests the presence of larger par-

ticles. But for reasons already discussed in Chapter 4 , no further attempt is made

to determine a unied grain model to include these two sets of results.

5.3 A model to explain the variationIt is apparent from the work of Levasseur-Regourd (1996) and Hadamcik and Levasseur-

Regourd (2003a) that comets exhibit different kinds of phase angle dependence on

polarisation. As already explained in last section, it is tried to explain these polari-

metric differences in terms of differences in grain size distribution.




In the present work , a parameter g has been introduced and estimated which

signies the relative abundance of coarser grains in different comets.

The sample of comets included in the present calculations have widely different

values of perihelion distances (q); four of them are non-periodic and the rest are

periodic (refer Table 5.1). If ’dynamical age’ is dened in terms of a meaningful

combination of some orbital parameters, naturally q will be an important parameter.

There are many ways of dening the dynamical age of a comet. However, in the

present case of non-periodic comets, q is chosen as the only important parameter

and an empirical relation is suggested of the type

g = Dqn (5.4)

to nd any possible relation between g and q ? Here the constants D and n can be

determined by rst linearising the equation and making a least square t into our

data for four non-periodic comets viz. Austin, Bradeld, Hyakutake and Levy. In

Figure 5.1 , log(−g) is plotted against log(q). It is clear that a straight line of the

form log(−g) = log(2 .5) + 23 log(q) ts the linearised data very well. Thus one can

write the following mathematical relations

g = −2.5q2/ 3 (5.5)

or

d log(N (s))d log s

= −2.5q2/ 3 (5.6)

This is the simple model which is suggested by present analysis of data containing

four non-periodic comets. However, if one wants to include periodic comets, one can

again assume a simple model, where the grain aging is multiplied by the number

of times the comet has revolved around the sun. This can be done by modifying

equation (5.5) to

g = −2.5q2/ 3 1(1 + ( k/T )m )

(5.7)

where k is a constant having dimension of time (in years), T is the period of the




comet in years and m is some unknown index. Clearly, for non-periodic comets,

equation (5.7) reduces to equation (5.5).

At this stage, one may want to determine k and m for periodic comets. Here, there

are four comets like Halley, Hale Bopp, Faye and Kopff. Unfortunately, for comets

Faye and Kopff, there are only 4 and 6 polarimetric data points respectively, from

which one has to calculate g. Therefore, there is no strong case for including these

two comets in the present analysis (justication as discussed in Section 5.2 ). As

a result in Figure 5.1 the log(−g) is plotted against log(q) values for Halley and

Hale Bopp only among the periodic comets.

However, Halley and Hale Bopp are two well-studied comets and taking their g

values into account one can nd the values of the two unknowns m and k as 0.12 and

375 years, respectively. This allows us to write the following equation for periodic

comets:

g = −2.5q2/ 3 1(1 + (375 /T )0.12)

(5.8)

However, the introduction of equation (5.8) at this stage is only exploratory. To sug-

gest, a model for periodic comets, one should determine the values of the unknowns

m and k from a sample of larger number of periodic comets.The meaning of Figure 5.1 is as follows: for non-periodic comets the ‘relative

abundance of coarser grains’ g and ’nearness to sun’ (or perihelion distance q) are

related by the equation g = −2.5q2/ 3. Thus, all the non-periodic comets lie along

the straight line log( −g) = log(2 .5) + 23 log(q). The t appears to be very good. The

effect of the Sun (measured by nearness to sun or perihelion distance) clearly causes

the relative abundance of coarser grains to increase.

The periodic comets Faye, Kopff, Halley and Hale-Bopp are not expected to fall onthis straight line. This is so because here the effect of the sun is not measured by

perihelion distance alone, but also by how many times the comet has revolved around

sun. For this case another model (equation 5.8) has been suggested. Thus, short-

periodic comets are expected to deviate more from this straight line as compared to

long-periodic comets. This is shown in Figure 5.1 . Comet Hale Bopp (period 4000

years) seems to be placed closer to the straight line as compared to Halley (period

76 years). The position of the comets Faye and Kopff are not to be taken seriously




-0.15

-0.1

-0.05

0

0.05

0.1

0.15

0.2

0.25

0.3

0.35

0.4

-0.7 -0.6 -0.5 -0.4 -0.3 -0.2 -0.1 0

l o g ( - g )

- - > F i n e r g r a i n s

log (q)

AustinBradfield

Hale-BoppHalley

HyakutakeLevy

Figure 5.1: Log of perihelion distance is plotted against log (−g), where g is the relative abundance of coarser grains. The straight line represents the equation

log(−g) = log(2 .5) +2

3 log(q)).



5.4:Discussion 82

as there are very few data points corresponding to them. Also these two being

periodic comets are not expected to fall on the straight line.

5.4 DiscussionIn the present work Mie Scattering theory has been used to match the observed

cometary polarisation data. With this theory one can generate polarisation values

for light scattered by compact spheres. However cometary particles are ’uffy ag-

gregates’ or porous, with irregular shapes. Because of the difficulties involved in

the calculations of scattering from porous particles, Mie calculations on spherical

particles are widely used as an approximation to the true situation. There havebeen many recent developments, however, in the eld of scattering by porous grains

which need to be mentioned here.

Greenberg and Hage (1990) originally proposed the existence of a large number

of porous grains in the coma of comets in order to explain the spectral emission

at 3.4 and 9.7 µm. Model calculations have been done by Hage and Greenberg

(1990) for particles with various porosities, sizes and compositions to generate dif-

ferent scattering properties. The typical properties of such porous particles areenhanced absorption and emission features, lower albedo, etc., compared to those

of Mie spheres. Dollfus(1989) discussed the results of laboratory experiments by

microwave simulation and laser scattering on various complex shapes with different

porosities. These results were later compared to the observed polarimetric data on

Halley’s comet. It was also pointed out that the observed circular polarisation in

the coma of various comets could be a good indicator of aligned elongated grains.

This view was further strengthened by Rosenbush et al.(1987) when they observed

circular polarisation in comet Hale Bopp. Xing and Hanner (1997) have carried out

elaborate calculations with porous grains of various shapes and sizes using Discrete

Dipole Approximation (DDA) method. The polarisation values so obtained were

compared with the observed polarisation data for various comets. The ’aggregate

structure’ considered by them to represent porosity, was found to suppress large

amplitude uctuations in polarisation as observed for single spheres. This work also

explained cometary negative polarisation in a more satisfactory manner. Further, it



5.4:Discussion 83

was concluded that the ’equivalent volume spheres’ is a poor approximation to the

polarisations caused by aggregates.

In one recent work Kerola and Larson (2001), used T-matrix formulation to calcu-

late polarisation properties of non-spherical particles and applied the results to the

polarimetric measurements of comet Hale Bopp.

These new approaches with porous aggregates and different shapes in general pro-

duced a better t of the observed polarisation data of various comets. Thus the

favoured grain model is now that of ’uffy’ grains with irregular shapes, rather than

Mie’s compact spheres. The uffiness may change as a function of size, the smaller

ones being almost spherical, but the larger ones having more of a uffy structure.

It is also to be noted that, any grain model which is suggested to explain cometary

polarisation should also be able to explain ’Spectral Energy Distribution’ (SED) in

the Near Infra Red (NIR) part of the spectrum. The cometary grain size distri-

bution function as discussed in the present work (with a possible dependence on

the dynamical age of the comet, in terms of grain aging) should have also some

implications on the observed SED in the NIR region. A recent work by Hanner

and Hayward (2003) discusses clearly the role of dust size distributions on the NIR

ux. The different slopes in the grain size distributions as considered by the authors

can be related to our g parameter which expresses richness of coarser grains. As

discussed by the authors, small grains are hotter and they contribute more to the

total emission. According to the present work, the dynamically newer comets are

richer in ne grains and, thus, one should now be able to distinguish them in terms

of their NIR ux.



References 84

References

A’Hearn M. F.1999,Recent Developments in the study of comets . In Asteroids,

comets, Meteors 1996 , COSPAR Colloqquium 10, pp17-28.


Chernova G.P., Kiselev N.N., Jockers K., 1993, Icarus , 103 ,144.

Delsemme A. H., 1987. In Symposium on diversity and similarity of comets , ESA

SP -278, p.19. Eds. Rolfe, E. J. & Battrick, B., ESA, Garching.

Dollfus A., 1989, A&A, 213 , 469.


Greenberg J. M. and Hage J. I. 1990, ApJ , 361 , 260.

Hadamcik E., and Levasseur-Regourd A.C., 2003a, JQSRT , 79-80 , 661.

Hadamcik E., and Levasseur-Regourd A.C., 2003b, A&A, 403 , 757.

Hage J. I. and Greenberg J. M., 1990, ApJ , 361 , 251.

Hanner M.S. and Hayward T. L., 2003, Icarus , 161 , 164.

Harker D.E., Wooden D.H.,Woodward C.E., Lisse C. M., 2002, ApJ , 580 , 579.

Hayward T.L., Hanner M.S., and Sekanina Z., 2000, ApJ , 538 , 428.

Kerola D. X. and Larson S. M, 2001, Icarus , 149 , 351.






Levasseur-Regourd A.C. and Hadamcik E., 2003, JQSRT , 79-80 , 903.



References 85

Levasseur-Regourd A.C., Hadamcik E., Renard J.B., 1996, A&A, 313 , 327.


Marsden, B.G. and Williams, G.V., 1995. In Catalogue of cometary orbits , 10thed., IAU Central Bureau for Astronomical Telegrams and Minor Planet Center




Mukai T., Mukai S., Kikuchi S., 1987, A&A, 187 ,650.

Rosenbush V. K., Shakhovskoj N. M., Rosenbush A.E., 1997, Earth, Moon &

Planets , 78 , 381.


242 , 496.


Sen A.K., 2001. In Small Telescope Astronomy in on Global Scale , IAU Colloquium

183, Kenting, Taiwan, 4-8 January, 2001, ASP Conference series, edts. Chen W.P,

Lemme C., Paczynski B, 246 , p275.

Xing, Z. and Hanner M.S 1997, A&A, 324 , 805.



Chapter 6

POLARISATION DATA OF

COMET LEVY 1990XX AND

APPLICATION OF T-MATRIXTHEORY

In this chapter, T-matrix theory is discussed. Then the polarimetric data of comet

Levy 1990XX is analysed using Mie and T-matrix theory. Finally, the negative

polarisation behaviour of comet Levy 1990XX is discussed.

6.1 T-matrix TheoryThe T-matrix method is a powerful exact technique for computing light scatter-

ing by nonspherical particles based on numerically solving Maxwell’s equations.This method was initially introduced by Waterman (1965, 1971) as a technique for

computing electromagnetic scattering by single, homogeneous nonspherical parti-

cles based on the Huygens principle. It is one of the most powerful and widely

used tools for rigorously computing electro magnetic scattering by single and com-

pounded nonspherical particles. An attractive feature of the T-matrix approach is

that it reduces exactly to the Mie theory when the particle is a homogeneous or

layered sphere composed of isotropic materials.

86




6.1:T-matrix Theory 87

The single scattering of light by a small volume element dv consisting of randomly

oriented, rotationally symmetric, independently scattering particles is completely

described by the ensemble averaged extinction, C ext and scattering, C sca , cross sec-

tions per particle and the dimensionless Stokes scattering matrix (van de Hulst,

1957):

F (Θ) =

a1(Θ) b1(Θ) 0 0

b1(Θ) a2(Θ) 0 0

0 0 a3(Θ) b2(Θ)

0 0 −b2(Θ) a4(Θ)

(6.1)

where Θ is the scattering angle , i.e., the angle formed by the incident solar ray’s

direction and the scattered ray’s direction. The observational phase angle is given

by α = 1800 −Θ.

For Mie particles , a1(Θ) = a2(Θ) and a3(Θ) = a4(Θ).

In the case of the single scattering regime, the degree of polarisation is given by:

p = −b1(Θ)a1(Θ)

(6.2)

The scattering matrix describes the transformation of the Stokes vector of the inci-

dent beam, Iinc

, into the Stokes vector of the scattered beam, Fsca

, provided thatboth Stokes vectors are dened with respect to the scattering plane (plane through

the incident and scattered beams):

I sca =C sca n0dv

4πR 2 F (Θ) I inc , (6.3)

where, n0 is the particle number density, and R is the distance from the small volume

element to the observation point. The Stokes vector is dened as a (4 ×1) column

having the Stokes parameters I ,Q,U and V as (van de Hulst, 1957):

I =

I

Q

U

V

(6.4)

Also there are special relations for the scattering angles 0 and π (van de Hulst, 1957;

Mishchenko & Hovenier, 1995).

a2(0) = a3(0), a2(π) = −a3(π), (6.5)



6.1.1:Theory 88

b1(0) = b2(0) = b1(π) = b2(π) = 0 , (6.6)

a4(π) = a1(π) −2a2(π) (6.7)

The ensemble-averaged absorption cross section per particle is dened as the differ-ence between the extinction and scattering cross sections:

C abs = C ext −C sca (6.8)

In computations for rotationally symmetric particles in random orientation, the

efficient approach is to expand the elements of the scattering matrix as follows (de

Haan et al., 1987, Mishchenko, 1991):

a1(Θ) =smax

s=0α s

1P s00(cosΘ) (6.9)

a2(Θ) + a3(Θ) =smax

s=2(α s

2 + α s3)P s22(cosΘ) (6.10)

a2(Θ) −a3(Θ) =smax

s=2(α s

2 −α s3)P s2,− 2(cosΘ) (6.11)

a4(Θ) =smax

s=0α s

4P s00(cosΘ) (6.12)

b1(Θ) =

smax

s=2 β s1P

s02(cosΘ) (6.13)

b2(Θ) =smax

s=2β s2P s02(cosΘ) (6.14)

where P smn (x) are generalised spherical functions (Gelfand et al., 1963; Hovenier &

van der Mee, 1983), and the upper summation limit, smax , depends on the desired

numerical accuracy of the expansions. Knowledge of the expansion coefficients α s1

to β s2 in equations (6.9)-(6.14) allows an easy calculation of the elements of the

scattering matrix for essentially any number of scattering angles.

6.1.1 Theory

Let us consider the scattering of a plane electromagnetic wave

E inc (R ) = E inco eik n inc .R , E inc

o .n inc = 0 , (6.15)

by a single nonspherical particle in a xed orientation with respect to the reference

frame, where k = 2πλ and λ is a free-space wavelength.



6.1.1:Theory 89

The incident and scattered elds are expanded in vector spherical functions M mn

and N mn as follows: (Tsang et al., 1985)

E inc

(R ) =

n max

n =1 .

n

m = − n[amn RgM mn (kR ) + bmn RgN mn (kR )], (6.16)

E sca (R ) =n max

n =1.

n

m = − n[ pmn M mn (kR ) + qmn N mn (kR )], |R | > r 0 (6.17)

where r 0 is the radius of a circumscribing sphere of the scattering particle and the

origin of the co-ordinate system is assumed to be inside the particle.

From the linearity of Maxwell’s equations and boundary conditions, the relation

between the scattered eld coefficients pmn and qmn on one hand and the incident

eld coefficients amn and bmn on the other hand is linear and is given by a transitionmatrix (or T matrix) T (Waterman 1971, Tsang et al. 1985) as follows:

pmn =n max

n =1.

n

m = − n[T 11

mnm n am n + T 12mnm n bm n ], (6.18)

qmn =n max

n =1.

n

m = − n[T 21

mnm n am n + T 22mnm n bm n ], (6.19)

In compact matrix notation, equation (6.18) and (6.19 ) can be written as:

p

q= T

a

b=

T 11 T 12

T 21 T 22

a

b(6.20)

Equation (6.20) forms the basis of the T-matrix approach. Since the expansion

coefficients amn and bmn of the incident plane wave can be easily calculated using

closed-form analytical expressions, the knowledge of the T-matrix for a given scat-

terer allows the computation of the scattered eld via equations (6.17)- (6.19). A

fundamental feature of the T-matrix approach is that the elements of the T-matrix

are independent of the incident and scattered elds and depend only on the shape,

size parameter and refractive index of the scattering particle as well as on its orien-

tation with respect to the reference frame.

The T-matrix computed for an arbitrary orientation of a non spherical particle

can be directly used in an analytical computation of the scattering characteristics

of randomly oriented particles (Mishchenko, 1991). The extinction and scattering

cross-sections averaged over the uniform orientation distribution of a non spherical



6.1.1:Theory 90

particle are given by the following simple formulas:

C ext = −2πk2 Re

n max

n =1.

n

m = − n[T 11

mnmn + T 12mnmn ], (6.21)

C sca = 2πk2

n max

n =1

n max

n =1

n

m = − n

n

m = − n

2

i=1

2

j =1 |T ijmnm n |2, (6.22)

For a spherical particle with spherically symmetric internal structure,

T 11mnn = −δnn bn , (6.23)

T 22mnn = −δnn an , (6.24)

T 12mnn = T 21

mnn = 0 , (6.25)

where an and bn are the Mie coefficients, if the particle is homogeneous, and other

analogs, if the particle is radially inhomogeneous.

The standard method for computing the T-matrix for a nonspherical particle is

based on the Extended Boundary Condition Method (EBCM) (Waterman, 1971;

Barber & Yeh, 1975). In addition to the expansions of the incident and scattered

elds given by equations (6.16) and (6.17), the internal eld is also expanded in

vector spherical functions:

E int (R ) =n max

n =1

n

m = − n[cmn RgM mn (m r kR ) + dmn RgN mn (m r kR )], (6.26)

where m r is the refractive index of the particle relative to that of the surrounding

medium.

The relation between the expansion coefficients of the incident and internal elds is

linear and is given by

ab

= Q11

Q12

Q21 Q22cd

, (6.27)

where the elements of the matrix Q are two-dimensional integrals which must be

numerically evaluated over the particle surface and depend on the particle size,

shape, refractive index and orientation.

The scattered eld coefficients are expressed in the internal eld coefficients as

p

q = −RgQ 11 RgQ 12

RgQ 21 RgQ 22

c

d , (6.28)



6.1.3:Size Distribution Function 91

where, the elements of the RgQ matrix are two dimensional integrals over the par-

ticle surface.

Comparing equations (6.27) and (6.28) with equation (6.20), it can be written as

T = −RgQ [Q ]− 1, (6.29)

Using general formulas, the matrices Q and RgQ for particles of any shape can be

calculated (Tsang et al., 1985). The formulas become much simpler for rotationally

symmetric particles provided that the axis of particle symmetry coincides with the

z axis of the coordinate system.

6.1.2 Particle shapes and sizesT-matrix can be applied to any rotationally symmetric particle having a plane of

symmetry perpendicular to the axis of rotation (viz., spheroids, nite circular cylin-

ders, even-order Chebyshev particles etc.). Spheroids are formed by rotating an el-

lipse about its minor axis (oblate spheroid) or major (prolate spheroid) axis. Their

shape in the spherical coordinate system is described by the equation:

r (θ, φ) = a sin2

θ +a2

b2 cos2

θ

− 1/ 2

, (6.30)where θ is the polar angle, φ is the azimuth angle, b is the rotational (vertical)

semi-axis, and a is the horizontal semi axis. The shape and size of a spheroid can be

specied by the axial ratio EP S (= a/b ) and the equal-surface-area-sphere radius,

r s (or the equal-volume-sphere radius r v). The axial ratio, EPS > 1 for oblate

spheroids, EPS < 1 for prolate spheroids, and EP S = 1 for spheres.

Similarly, the shape and size of a nite circular cylinder can be specied by the ratio

of the diameter to the length, D/L , and the equal-surface-area-sphere radius, r s (or

the equal-volume-sphere radius r v). D/L < 1 for prolate cylinders, D/L = 1 for

compact cylinders, and D/L > 1 for oblate cylinders. It is also possible to specify

the shape and size of Chebyshev particles.

6.1.3 Size Distribution Function

To average the optical cross sections and the expansions coefficients in equation (6.9)

- (6.14) over a size distribution, it is necessary to evaluate numerically the following



6.1.3:Size Distribution Function 92

integrals:

C sca = r 2

r 1

n(r )drC sca (r ), (6.31)

C ext = r 2

r 1 n(r )drC ext (r ), (6.32)

α si =

1C sca

r 2

r 1

n(r )drC sca (r )α si (r ), i = 1 , ...., 4, (6.33)

β si =1

C sca r 2

r 1

n(r )drC sca (r )β si (r ), i = 1 , 2, (6.34)

where n(r )dr is the fraction of particles with equivalent-sphere radii between r and

r + dr , and r 1 and r 2 are the minimal and maximal equivalent-sphere radii in the

size distribution. The distribution function n(r ) is normalised to unity as follows:

r 2

r 1

n(r )dr = 1 , (6.35)

Several analytical functions are often used to model natural particle size distri-

butions. The T-matrix theory allows one to choose from the following set of six

analytical size distributions:

• The modied gamma distribution

n(r ) = constant ×rα

exp(−αr γ

γr γ c ), (6.36)

• The log normal distribution

n(r ) = constant ×r − 1exp −(lnr −lnr g)2

2ln 2σg, (6.37)

• The power law distribution

n(r ) =constant ×r − 3, r1 ≤ r ≤ r 2,

0, otherwise,(6.38)

• The gamma distribution

n(r ) = constant ×r (1− 3b)/b exp −rab

, b (0, 0.5); (6.39)

• The modied power law distribution

n(r ) =

constant, 0 ≤ r ≤ r 1,

constant ×(r/r 1)α , r1 ≤ r ≤ r 2,

0, r2 < r,

(6.40)



6.2:Grain characteristics of comet Levy 1990 XX 93

• The modied bimodal log normal distribution

n(r ) = constant ×r − 4 exp −(lnr −lnr g1)2

2ln 2σg1+

γexp −(lnr −lnr g2)2

2ln 2σg2, (6.41)

Important characteristics of a size distribution are the effective radius r eff and

effective variance veff dened as (Hansen and Travis, 1974):

r eff =1G

r 2

r 1

rπr 2n(r )dr, (6.42)

veff =1

Gr ef f

2

r 2

r 1

(r −r ef f )2πr 2n(r )dr, (6.43)

where,

G = r 2

r 1

πr 2n(r )dr, (6.44)

6.2 Grain characteristics of comet Levy 1990 XXPolarimetry in the continuum is a good technique to study the nature of cometary

dust grains. Many authors (Bastien et al, 1986; Kikuchi et al, 1987, 1989; Lamyet al, 1987, Le Borgne et al., 1987; Mukai et al., 1987; Sen et al., 1991a, 1991b;

Das et al., 2004 etc.) have studied linear and circular polarisation measurements of

several comets. The spherical grain characteristics of comets can be studied using

Mie scattering theory. One can nd out polarisation values for light scattered by

compact spheres using this theory and can match the result with observed polari-

sation data (Sen et al., 1991a, 1991b; Das et al., 2004). But cometary particles are

’uffy aggregates’ or porous, with irregular shapes (Greenberg & Hage, 1990). The

measurement of circular polarisation of comet Hale-Bopp (Rosenbush et al., 1997)

also reveals that cometary dust grains must be composed of non-spherical particles.

Xing & Hanner (1997) have carried out calculations with porous grains of different

shapes and sizes with Discrete Dipole Approximation (DDA) method. In order to

study the irregular grain properties of comets, T-matrix theory (Mishchenko, 1991,

1998) has been used by many investigators (Kolokolova et al., 1997; Kerola & Lar-

son, 2001). Using T-matrix Theory, Kerola & Larson (2001) calculated polarisation



6.2.1:Using Mie Theory 94

for non-spherical particles and compared the results with the polarimetric measure-

ment of comet Hale-Bopp. They have found that prolate grains are more satisfactory

than other shapes in comet Hale-Bopp.

The polarimetric data of comet Levy 1990 XX has been taken from Chernova et

al. (1993). Since the polarimetric data is only available at λ = 0 .485µm, the

analysis is restricted to that wavelength. Kerola & Larson (2001) have analysed

the comet Hale-Bopp at 0 .485µm and 0.684µm and have got same set of parameters

that can characterise the polarisation properties of comet Hale-Bopp. In the present

paper, the irregular grain properties of comet Levy 1990 XX have been studied using

Mishchenko’s (1991, 1998) T-matrix code. The result obtained from the T-matrix

theory is compared with Mie theory results (as already calculated in Chapter 5 ).

6.2.1 Using Mie Theory

Mie theory provides an analytic solution to the general scattering problem for spheres

and correctly describes the interaction of light with dust grains that are small com-

pared with the wavelength of light. Several investigators ( Mukai et al., 1987; Sen

et al., 1991a, 1991b; Chernova et al., 1994; Joshi et al., 1997; Kiselev & Velichko,1998) have studied different comets and tried to analyse the dust grain behaviour

of comets using Mie theory. The dust size distribution function N (s) for Halley

(δ = 2 .2gcm− 3) as derived in Chapter 4 from the work of Lamy et al.(1987)is :

logN (s) = a(logs)2 + b(logs) + c, (6.45)

where, a = −0.2593, b = −4.422, c = −15.06.

The lower and upper limit of the grain sizes are xed at 0.001 µm and 20 µm.Using Mie theory, one can determine the best t values of ( n, k ), at which the sum

of squares of difference between expected and observed values of polarisation ( χ 2-

value) becomes minimum.

As already discussed in Chapter 5 , the composition of dust grains are less likely to

differ from comet to comet. So the composition (n, k ) is taken to be xed and the size

distribution ( a, b) is varied alone. The values of a and b emerging out from present

work are (-0.049, -3.17) (Ref. Table 5.1 ). The χ 2- value for this analysis is found to





6.3:Discussions 96

6.3 DiscussionsT-matrix theory is a powerful tool to study the polarimetric behaviour of comets

for irregularly shaped grains. So, Mie theory will give less exact results, if grains are

irregular. Also, one can note that χ 2- values emerging out from Mie theory and T-

matrix theory are 29.4 and 5.22 respectively. So, it is clear that T-matrix calculation

gives better t to the observed data. In Fig.6.3 , the expected polarisation curve

is plotted on observed data points for both spherical grains (based on Mie theory )

and prolate grains (based on T-matrix theory). Thus one can see that prolate grains

can give more satisfactory results in comet Levy 1990 XX. Cometary grains may be

of other shapes also. But in the present work, a simple model has been considered.

The negative polarisation behaviour of a comet is very interesting. Many comets

show negative polarisation beyond 157 0 scattering angle (Kikuchi et al., 1987; Cher-

nova et al., 1993; Ganesh et al., 1998 etc.). Several authors (Greenberg & Hage,

1990; Muinonen, 1993) have discussed the cause of negative polarisation in comet.

The mechanism of coherent back scattering proposed by Muinonen(1993) has been

used to explain the negative polarisation. The uffy aggregate model originally pro-

posed by Greenberg and Hage (1990) and later adopted by Xing and Hanner (1997)are also preferred for the study of negative polarisation in comets. Many investiga-

tors (Mukai et al., 1987; Sen et al., 1991a, 1991b; Joshi et al., 1997; ) have generated

expected polarisation curve using Mie theory that shows negative polarisation

beyond 1570. The expected negative polarisation curve has not been found in comet

Hale-Bopp using T-matrix theory (Kerola and Larson, 2001). Their analysis has

been restricted for θ ≤ 1600. Kerola & Larson (2001) also concluded that combi-

nation of viewing geometry effects and enhanced multiple scattering might providea quantitative explanation of the negative polarisation beyond 160 0. In the present

work, it is also interesting to note that both Mie and T-matrix theory give negative

polarisation curve in comet Levy 1990 XX. Taking r ef f = 0 .218µm, vef f = 0 .0036

and EP S = 0 .486 at λ = 0 .485µm, one can generate negative polarisation curve us-

ing T-matrix theory for θ ≥1570. But it is also important to study the uffy grains

with irregular shapes and enhanced multiple scattering which may well explain the

negative polarisation in comets.



6.3:Discussions 97

-10

-5

0

5

10

15

20

120 130 140 150 160 170 180

P o

l a r i s a t i o n

( i n % )

Scattering Angle (in degrees)

Figure 6.1: The observed polarisation values of comet Levy 1990 XX at λ =0.485µm (Chernova et al., 1993). The solid line represents the theoretical values for

Mie type scattering with (n, k ) = (1 .390, 0.026).



6.3:Discussions 98

-2

0

2

4

6

8

10

12

14

16

120 130 140 150 160 170 180

P o

l a r i s a t i o n

( i n % )


Figure 6.2: The solid line represents the good t of T-matrix polarisation calcu-lations at λ = 0 .485µm using prolate spheroids ( r ef f = 0 .218µm, veff = 0 .0036 and

EP S = 0 .486) with (n, k ) = (1 .63, 0.00003) (for olivine) .



6.3:Discussions 99

-10

-5

0

5

10

15

20

120 130 140 150 160 170 180

P o l a r i s a

t i o n ( i n % )


Prolate grainsSpherical grains

Figure 6.3: Comparison of Mie theory and T-matrix theory results. The dottedline represents the best t polarisation values for spherical grains obtained from Mie

theory and the solid line for prolate grains obtained from T-matrix theory.



References 100

ReferencesBarber P. and Yeh C., 1975, Appl. Opt. , 14 , 2864.


Chernova G.P., Kiselev N.N., Jockers K., 1993, Icarus , 103 ,144.

Das H. S., Sen A. K., Kaul C. L., 2004, A&A, 423 , 373.

de Haan J. F., Bosma P. B. and Hovenier J. W., 1987, A & A, 128 , 1.

Delsemme A. H., 1987, In Symposium on diversity and similarity of comets , ESA

SP -278, p.19, eds. Rolfe, E. J. & Battrick, B., ESA, Garching.

Eaton N., Scarrott S.M., Gledhill T.M., 1992, MNRAS , 258 , 384.

Ganesh S., Joshi U. C., Baliyani K. S., Deshpande M. R., 1998, A& AS , 129 , 489

Gelfand I. M., Minlos R. A. and Shapiro Z. Ya., 1963. In Representations of the

Rotation and Lorentz Groups and their Applications , Pergamon Press, Oxford.

Greenberg J. M. & Hage J. I., 1990, ApJ , 361 , 260.

Greenberg J. M. & Li A. 1996, A& A, 309 ,258.

Hanner M. S, Lynch D. K. & Russell R. W., 1994, ApJ , 425 , 275.

Hansen J. E. and Travis L. D., 1974, Space Sci. Rev. , 16 , 527.

Hovenier J. W. and van der Mee C. V. M., 1983, A & A, 128 , 1.

Joshi U.C., Baliyan K.S., Ganesh S., Chitre A., Vats H.O., Deshpande M.R., 1997,

A&A, 319 , 694.

Kerola D. X. & Larson S. M. 2001, Icarus , 149 , 351.

Kikuchi S., Mikami Y., Mukai T., Mukai S., Hough J.H., 1987, A&A, 187 , 689.



References 101

Kikuchi S., Mikami Y., Mukai T., Mukai S., 1989, A&A, 214 , 386.

Kiselev N.N & Velichko F.P., 1998, Icarus , 133 , 286.

Kolokolova L., Jockers K., Chernova G., 1997, Icarus , 126 , 351.



Levasseur-Regourd A.C., Hadamcik E., Renard J.B., 1996, A&A, 313 , 327.

Lynch D., Russel R., Hackwell J., Hanner M., Hammel H., 1992, Icarus , 100 , 197.

Manset N., Bastien P., 2000, Icarus , 145 , 203.

Mazets E.P., Sagdeev R.Z., Aptekar R.L., Golenetskii S.V., Guryan Yu.A., Dy-

achkov A.V., Ilyinskii V.N., Panov V.N., Petrov G.G., Savvin A.V., Sokolov I.A.,

Frederiks D.D., Khavenson N.G., Shapiro V.D., Shevchenko V.I., 1987, A&A, 187 ,

699.

Mishchenko M. I., 1991, J. Opt. Soc. Am. A , 8, 871; errata 1992, 9, 497.

Mishchenko M. I. and Hovenier J. W., 1995, J. W. Opt. Lett. , 20 , 1356.

Mishchenko M. I. & Travis L. D., 1998, J. Quant. Spect. Rad. Transf. , 60 , 309.

Muinonen K., 1993, In IAU Symposium 160. Asteroids, Meteors, Comets , pp 271-

296.


1991] Sen A.K., Deshpande M.R., Joshi U.C., Rao N.K., Raveendran A.V., 1991a,

A&A, 242 , 496.


Tsang L., Kong J. A. and Shin R. T., 1985. In Theory of Microwave Remote

Sensing , Wiley, New York.



References 102

van de Hulst H. C., 1957. In Light Scattering by Small Particles , John Wiley and

Sons, New York.

Waterman P. C., 1965, Proc. IEEE , 53 , 805.

Waterman P. C., 1971, Phys. Rev. D , 3, 825.

Xing, Z. & Hanner M. S. 1997, A&A, 324 , 805.



Chapter 7

POLARIMETRIC STUDIES OF

DARK CLOUDS

This chapter begins with the basic introduction of dark clouds, which are potential

sites of star formation. Then the statistical distribution of the degree of polarisation

and position angle observed for stars background to such clouds are presented. The

relation between the observed polarisation and ambient physical conditions in the cloud are also discussed. Finally, the spatial distribution of the polarisation and

position angle values are studied.

7.1 IntroductionThe small compact dark clouds or ’Bok Globules’ as they are also known as, are be-

lieved to be the ideal sites for star formation (Bok & Reilly 1947 ). Such clouds have

been catalogued by Bernard (1927), Lynds (1962) and more recently by Clemens &

Barvainis (1988).

These clouds are undergoing gravitational collapse and eventually may form stars.

The ambient magnetic eld plays a key role in the collapse dynamics by directing the

outows, impeding the plasma movement across magnetic eld and in many other

ways. Owing to this, there have been several attempts in past to measure strength

and geometry of the magnetic eld within the cloud. Astronomers have been using

103




7.1:Introduction 104

background star polarimetry as a tool to understand the ambient magnetic eld

and study the star formation dynamics in the cloud (Vrba et al 1981; Joshi et

al. 1985; Goodman et al 1989; Myers & Goodman 1991; Kane et al 1995; Sen

et al. 2000, to mention a few). This technique has an underlying assumption

that, the light from the background stars are scattered in the forward direction

by the magnetically aligned dichroic dust grains in the cloud. Davis & Greenstein

(1952) rst worked out a procedure showing how grain alignments are possible by

magnetic eld. Several modications of this mechanism and various other alignment

mechanisms are presently discussed in the literature (for a detail review on this please

see Lazarian et al. (1997)).

It is normally expected that, grains which cause polarisation, should also be re-

sponsible for the extinction observed for the background stars. However, Goodman

et al (1995) observed a lack of dependence of polarisation with extinction and this

has questioned the validity of polarisation as a tracer of magnetic eld in these

clouds. More recently Sen et al (2000) have mapped eight star forming clouds CB3,

CB25, CB39 , CB 52, CB54, CB58, CB62 and CB246 in white light polarisation

and commented on the possible star formation dynamics there.

With the above background, in this chapter a detail analysis of the polarisation

images of the above eight clouds is carried out. Attempts were made to understand

whether the ambient physical parameters like temperature and turbulence have any

role on the observed polarisation value. Further the projected angular distances

(henceforth ’radial distance’) of the background stars from the cloud center were

estimated, for the eight clouds as observed by Sen et al (2000). Hence the data

was analysed , to nd whether the polarisation values observed for these stars are

anyway related with these distances ?





7.2:The statical distribution of the degree of polarisation and position angle in a given cloud 106

a dark cloud with a given sample of stars, some stars are neither foreground nor

background to the cloud, but lying a bit outside the periphery of the cloud. This

happens because shape of the cloud is mostly irregular and does not evenly cover the

area of the rectangular detector. So these stars also contribute to the polarisation

data, and represent simple interstellar polarisation. Such stars probably contribute

largely to the second Gaussian component, as in the present case all the clouds are

quite nearby and one should not have many stars foreground to the clouds. It is

also likely that (i)the polarisation produced within the cloud has direction different

from that produced in the interstellar medium. In the IS medium one should have

polarisation mostly aligned along the direction of galactic magnetic eld (coinciding

with the direction of galactic plane ) or (ii) within the same cloud itself there may

be no-uniform magnetic elds. Such features can be studied from the histogram

plot of θ. Myers & Goodman (1995) made a very detailed analysis on the dispersion

in the direction of polarisation for 15 dark clouds, ve clusters and six complexes.

It was shown that the bimodal distributions can be explained, through a model,

where there exist two components in magnetic eld one uniform and another non-

uniform. The non-uniform part has an isotropic probability distribution of direction,

a Gaussian distribution of amplitudes and N correlation lengths along the line of

sight. This model was applied to the cloud L1755 by Goodman et al. (1995) to

explain the distribution of direction of polarisation vectors.

As can be seen from Figure 7.2 , almost all the clouds show a single peak in the

distribution of θ values, which is somewhat very close to the direction of galactic

magnetic eld (θG ). In clouds CB52 and CB58 there may be small exception showing

two peaks in θ distribution, but it is not very signicant. A closer look at the

histogram depicts that the peak in θ values for all the clouds lies within 1σθ (as

listed in Table 7.1 ) from the direction of galactic plane θG (representing magnetic

eld).




Table 7.1: For various CB clouds, the number of stars, average polar-

isation, average position angle, dispersion, dust and gas temperatures,

turbulence , difference |θG −θav | and cloud groups are shown

Name of No. of pav θav σθ T d (0 K ) T g (0 K ) ∆ V |θG −θav | Cloud

the cloud stars (kms − 1 ) Group

CB3 31 1.41 65.43 15.40 112 11.27 3.08 23.57 C

CB25 21 2.35 150.89 5.91 153 8.90 0.70 5.89 A

CB39 21 1.95 150.27 35.35 106 9.45 2.05 0.73 ACB52 16 1.27 77.81 51.95 111 9.76 4.03 75.19 C

CB54 48 0.86 115.96 37.85 97 11.08 4.51 36.04 C

CB58 29 1.81 101.06 43.01 110 11.22 1.67 49.94 A

CB62 13 0.70 67.64 45.80 107 – – 22.36 ?

CB246 14 1.92 67.43 19.48 – 9.50 1.62 14.57 A

CB4 80 2.84 70.55 25.71 114 11.77 0.57 19.45 A




Figure 7.1: Histogram showing the number ( N stars ) distribution of stars having Rice corrected polarisation ( price ) values in different ranges for various clouds.





7.3.1:The dependence of observed polarisation on dust and gas temperature 110

A similar conclusion can also be arrived at by looking at Table 7.1 , where one nds

the σθ and |θG −θ| values are very close to each other. This observation suggests

that the direction of IS magnetic eld and that of the magnetic eld within the cloud

(responsible for grain alignment) may be the same or these two differ only within

1σ. The eld responsible for the alignment of grains, therefore, can be assumed to

be related to the galactic magnetic eld.

7.3 Observed polarisation and ambient physical

conditions in the cloud

7.3.1 The dependence of observed polarisation on dust and

gas temperature

The light from stars background to the cloud is generally found to be polarised.

This happens due to the scattering of the light from the background stars by the

aligned dichroic grains present in the cloud. It is believed that the alignment is

resulted from an interaction between the rotational dynamics of the grains and the

ambient magnetic eld. This mechanism called paramagnetic relaxation was origi-

nally suggested by Davis & Greenstein (1951). It can be shown that the percentage

of polarisation ( p%) as expected by this mechanism can be expressed as (Vrba et al.

1981):

p(%) = 67F Av (7.2)

where Av is total visual extinction and the expression for F can be found from Jones& Spitzer (1967) :

F =χ B 2

75aωn(

2πmkT g

)1/ 2(γ −1)(1 −T d/T g) (7.3)

where χ is the imaginary part of the complex susceptibility of the grains, ω is the

angular velocity of rotation, T d and T g are the dust and gas (kinetic) temperatures, B

is magnetic eld, n is gas density in the vicinity of grain (generally taken as Hydrogen

gas density), m is gas molecular mass, k is Boltzman constant, γ = (1 / 2)[(b/a )2 +1],




b and a are short and long axes of the grains . Further it is known that (Davis &

Greenstein 1951; Purcell 1979) :

χω = 2 .6 10− 12T − 1d

Therefore one can write a simplied expression for p(%) as :

p(%)∼B 2

n1

T g(

1T d −

1T g

)Av (7.4)

The total extinction Av in a cloud can be related to the gas (hydrogen) density

in the cloud. The relation Av ∼n(H ) seems to be true for all parts of the cloud

and this relation has been experimentally veried except at very high opacities

(Jenkins & Savage 1974). Subsequently many authors (Dickman 1978; Gerakins

et al. 1995) used such a relation to study various physical parameters of clouds.

Therefore assuming classical Davis & Greenstein mechanism one may obtain from

the equation (7.4):

p(%)∼B 2 1

T g(

1T

d−

1T

g

) (7.5)

However, the classical Davis & Greenstein Mechanism has undergone many modica-

tions and various other grain aligning mechanisms are now being used to explain the

background star polarisation (Cugnon 1985; Lazarian 1997; Lazarian et al. 1997).

In the present work restricting oneself to the simplest classical model of Davis &

Greenstein, one should get the polarisation observed in a cloud to be related to the

dust and gas temperature ( T d and T g respectively) by the equation (7.5).

In the present analysis average polarisation values for nine (=8+1) clouds are avail-able. One can study the dependence of these polarisation values on the ambient

magnetic eld B , dust and gas temperatures ( T d and T g). Myers & Goodman

(1991) have studied the distribution of polarisation direction and line of sight mag-

netic eld component (as obtained from Zeeman measurement) for 15 dark clouds,

5 clustures and 6 complexes. The relation between polarisation direction and mag-

netic eld seems to be quite complicated. Since, the magnetic eld information on

most of the clouds considered here are not available, a study of the relation between






These will clearly defeat the purpose of analysing the polarising properties of the

cloud. With this justication only simple unweighted averages of p and θ values are

considered for this analysis.

In Figure 7.3 , the average polarisation ( pav ) values are plotted against the T 1

values. For CB62 and CB246, T 1 values were not calculated as data was not available

from Clemens et al. (1991). As can be clearly seen from Figure 7.3 , the plot does

not suggest any relation between pav and T 1 as is expected from equation (7.6).

Lazarian et al. (1997) in their work on the dark cloud L1755 tried to explain

the polarimetric data in terms of grain alignment mechanisms other than Davis &

Greenstein. Considering the grains to be of super-paramagnetic material (with a

justication from Goodman & Whittet 1995), the authors suggested that the degree

of Davis & Greenstein alignment should depend on ( T d/T m ) where T m = ( T d + T g)/ 2

or the average of of dust and gas temperatures. Thus one should have

p(%)∼(T d

(T g + T d))

Based on above a plot of pav versus T d(T g + T d ) ( denoted by T 2) is made as in Figure

7.4 . This plot also does not show any systematic dependence of polarisation ontemperature (in terms of the parameter T 2). However, if one excludes the data

corresponding to CB4, it appears that a straight line ( p∼T 2) may be tted. At

least compared to Figure 7.3 , the present plot in Figure 7.4 (excluding CB4)

shows some indications for an increase in p with T 2, as expected. Also there can be

reasons for the exclusion of data corresponding to CB4, where polarisation values

were obtained in V lter rather than in white light as in all other cases. The

polarisation in white light is always lower than what is observed through band passlters (as polarisation at different wavelengths combine vectorially to give lower net

average polarisation) . At this stage it may be also noted that, there are mechanisms

other than Davis- Greenstein one, which are now being used by several authors to

explain polarisation caused by aligned grains. These include Purcell alignemnt,

alignment by radiation torque, mechanical alignment of suprathermally rotating

grains (for a detailed review please see Lazarian et al 1997).






0.8

1

1.2

1.4

1.6

1.8

2

2.2

2.4

2.6

2.8

3

0.895 0.9 0.905 0.91 0.915 0.92 0.925 0.93 0.935 0.94 0.945

p a v

T2

cb3cb4

cb25

cb39cb52cb54cb58

Figure 7.4: The average of observed polarisation ( pav ) versus T 2(= T d(T g + T d ) ) for

various clouds.




-0.2

0

0.2

0.4

0.6

0.8

1

1.2

0.5 1 1.5 2 2.5 3 3.5 4 4.5 5

l n p a

v

∆ V

CB3CB4

CB25CB39

CB52CB54CB58

CB246

Figure 7.5: The log of average of observed polarisation ln( pav ) are plotted againstthe turbulence ∆ V for various clouds. The line of best t ln ( p) = 1 .0831−0.2424∆V

is shown along with.




5

10

15

20

25

30

35

40

45

50

55

8.5 9 9.5 10 10.5 11 11.5 12

σ θ

Tg

cb3cb4

cb25

cb39cb52cb54cb58

cb246

Figure 7.6: The dispersion in the direction of polarisation vectors ( σθ) are plottedagainst gas temperatures ( T g) for different clouds



7.3.2:The dependence of polarisation on the turbulence in the cloud 118

7.3.2 The dependence of polarisation on the turbulence in

the cloud

In the present analysis it is observed that the average polarisation pav

varies sub-

stantially from cloud to cloud which have different physical conditions as listed

by Clemens et al (1991). These authors also listed 12CO line width (in terms of

∆ V km sec− 1) values, which are assumed to be good indicators of turbulence

within the cloud (listed in Table 7.1 ). Based on this the authors have also clas-

sied the clouds into three groups : A ( T < 8.5 K and ∆ V < 2.5 km sec − 1 ), B

(T > 8.5K ) and C (T < 8.5K and ∆ V > 2.5 km sec − 1).

One may expect the turbulence to disturb the grain alignment, causing a reductionin the observed polarisation values. And when the turbulence becomes too high no

alignment may be possible. In the line of sight there may be several independent

directions of alignment causing a net depolarisation and resulting a low value of

observed polarisation. In this scenario an empirical relation of the type p = a∗exp(−∆ V.b) may be used to analyse the present situation. Here as the turbulence

becomes too high, grain alignment will be completely disturbed and one should get a

zero value for polarisation, even if other parameters (contained in a) are favourable toproduce high polarisation. On the other hand if no turbulence is present, one can not

get 100 % polarisation as the other parameters will decide the minimum observable

polarisation (decided by the value of a). The above equation p = a∗exp(−∆ V.b)

can be linearised and by the method of least-square one may t the following curve

to data

ln ( p) = 1 .0831−0.2424∆ V (7.7)

or, p = 2 .95∗exp(−0.24∆ V )

The above relation suggests a maximum value 2 .95% for background star polari-

sation. Figure 7.5 shows a plot of ln ( p) versus ∆ V along with the above line of

best t (equation (7.7)) for all the clouds except CB62 for which data is not avail-

able. The data on CB4 is also included from Kane et al. 1995 in this plot. In

Figure 7.5 a clear trend is observed where the average polarisation decreases with

increase in turbulence ∆ V . This can be clearly explained, as one knows the turbu-




lence present in the cloud can be held responsible for disturbing the grain alignment

causing lowering of polarisation values. However, in Figure 7.3 and Figure 7.4

where pav has been plotted across some meaningful function of T , no such clear

relation exists. But one may note that, if pav has a stronger dependence on ∆ V as

compared to T , then one can not explore the relation between pav and functions of

T from Figure 7.3 and Figure 7.4 . To analyse this situation little further, one

may study the relation by plotting data points ln ( pav /T 2) against ∆ V , which will

remove the effect of temperature from the observed polarisation. A new straight

line ln( pav /T 2) = 1 .1848 −0.2457∗∆ V may be tted on this new set of data with

no further reduction in tting error. Also one may note in the present case, cor-

responding to CB246 there will be no data point. Therefore, this situation is not

considered any further.




5

10

15

20

25

30

35

40

45

50

55

0.5 1 1.5 2 2.5 3 3.5 4 4.5 5

σ θ

∆ V

cb3cb4

cb25

cb39cb52cb54cb58

cb246

Figure 7.7: The dispersion in the direction of polarisation vectors ( σθ) are plottedagainst amount of turbulence ( ∆ V ) for different clouds




0.5

1

1.5

2

2.5

3

5 10 15 20 25 30 35 40 45 50 55

p a v

σ θ

cb3cb4

cb25

cb39cb52cb54cb58cb62

cb246

Figure 7.8: The average of observed polarisation ( pav ) are plotted against variance ( σθ) in the direction of polarisation vector




0.5

1

1.5

2

2.5

3

0 10 20 30 40 50 60 70 80

p a v

|θ G -θ |

cb3cb4

cb25cb39cb52cb54cb58cb62

cb246

Figure 7.9: The average of observed polarisation ( pav ) are plotted against |θG −θav |



7.3.3:The dependence of direction of polarisation vector on temperature and turbulence 123

7.3.3 The dependence of direction of polarisation vector on

temperature and turbulence

In the previous sub-section it was observed that the turbulence present in a cloud

can inuence the average polarisation values observed in the cloud. Thus one may

also expect the turbulence to disturb the direction of polarisation vector θ observed

within the cloud. With this aim one may study whether dispersion in position angle

( measured by variance σθ) has any dependence on T g and ∆ V ? To study the effect

of gas kinetic temperature ( T g) and turbulence (∆ V ), in Figure 7.6 and Figure

7.7 the variance in polarisation vector σθ for various clouds are plotted across the

gas temperature ( T g) and the turbulence (∆ V ) respectively. The value of variance inpolarisation vector ( σθ), seem to be unrelated to the gas kinetic temperature ( T g).

However, one can see there is a faint tendency for the amount of variance σθ to

increase with the rise in turbulence (∆ V ).

The dispersion ( σθ) in the direction of polarisation vector should be indicative of

the non-uniformity in the direction of the magnetic eld over different parts of the

cloud. Now since this non-uniformity is observed in a plane perpendicular to the

line of sight, one can also expect non-uniformity of same scale to be present alongthe line of sight. A random variation in the direction of magnetic eld should

reduce the value of observed polarisation, averaged over the line of sight. The dust

particles in a cloud can in general be expected to be aligned by uniform interstellar

magnetic eld. In that case one should have lower value of variance in the direction

of polarisation. Also the average value of polarisation in the cloud should be close

to the interstellar polarisation value in that part of the sky. But in situations

where there exist additional aligning mechanisms (operating within the cloud likemolecular outow, etc.) one should get a higher dispersion (variance) in the direction

of polarisation . This will happen because the interstellar magnetic eld will act in

vectorial combination with those additional aligning forces in the cloud. A higher

value of dispersion in θ is also possible if there are irregularities (complexities) in

the magnetic eld structure, caused due to mechanisms intrinsic to the cloud.

Thus a high value of σθ in some clouds, should indicate that there are irregularities

in the structure of aligning forces. Also under such cases in these clouds, one should



7.4.1: A simple model for the polarisation introduced by the cloud 124

get lower values of average polarisation. In Figure 7.8 , pav has been plotted against

σθ, where one can see tendencies for a decrease in pav with the increase in σθ. In

fact the data seem to be distributed into two clusters, where two different straight

lines may be tted. The data points corresponding to the clouds CB4, CB39, CB52

and CB58 may be tted into a separate straight line as compared to other clouds.

These two groups of data points however, do not systematically fall in any of the

groups A, B, C as discussed earlier ( Cf. Table 7.1 ). One may try to explore the

physical properties of the two sets of clouds which are responsible for this observed

behaviour. This is planned for future work.

If grains are aligned by galactic magnetic eld, one should nd average pav in a cloud

to be higher where the difference between the galactic plane direction θG and θav ie

|θG −θav | is lower. To establish this idea in Figure 7.9 , pav has been plotted across

|θG −θav | for different clouds. Primarily it appears to be a scatter plot, but one can

nd tendencies for the increase in pav with the decrease in |θG −θav | as expected.

Here also one can notice that, the data points corresponding to the clouds CB4,

CB52 and CB58 can be tted into a separate straight line as compared to the other

clouds which t in a second straight line. One may note that CB52 and CB58 are

two such clouds which showed bimodal distributions for θ (Cf. Figure 7.2 and

Section 7.2), as compared to others.

From the above discussions and discussions in Section 7.3.1 and 7.3.2, it appears

that the presence of turbulence lowers the polarisation observed in a cloud and

thus can be accepted as one of the factors responsible for the non-uniformity in

magnetic eld, disturbing the grain alignment. As a result it can be concluded that

polarisation observed for stars background to a given cloud, is not independent of

the physical properties of that cloud. The work by Goodman et al. (1995) expressed

concern that, it seems the polarisation observed for stars background to a cloud is

independent of the cloud and not produced within the cloud.




7.4 The spatial distribution of the polarisation

and position angle values

7.4.1 A simple model for the polarisation introduced by

the cloud

The clouds which have been observed by Sen et al (2000) are nearby with distances

less than 600 pc (Clemens & Barvainis (1988)). As a result the polarisation observed

for these background stars can be assumed to consist of only two components:

1) polarisation introduced by the interstellar ( IS ) medium background to the cloud.

For the foreground stars as the cloud is nearby, one can neglect the polarisationcaused due to the IS medium between the cloud and the observer.

2) polarisation introduced by the cloud itself, which is believed to be optically

thicker.

It is assumed that the polarisation properties of the IS medium can be approximated

by a simple dichroic sheet polarizer. The transmission properties of a simple dichroic

sheet polarizer (aligned in an arbitrary direction by angle φ with respect to some

reference direction ) can be mathematically represented by the following MuellerMatrix (Kliger et al 1990; Shurcliff 1962)

A(φ) =12

(k1 + k2) (k1 −k2)c2 (k1 −k2)s2 0

(k1 −k2)c2 (k1 + k2)c22 + 2 s2

2k (√k1 −√k2)2c2s2 0

(k1 −k2)s2 (√k1 −√k2)2c2s2 (k1 + k2)s22 + 2 c2

2k 0

0 0 0 2k

(7.8)

where c2 = cos(2φ) ; s2 = sin (2φ); k = √k1k2 and k1 and k2 are the transmission

coefficients for light when the electric vector is parallel and perpendicular to the

optic axis of the polarizer.

It is assumed the light from the background star is initially unpolarized and so

it can be represented by the Stokes coloumn matrix (Shurcliff 1962; Stoke 1852)

S = {I 0 0 0}. If one assumes the IS medium to be a dichroic polariser with optic

axis making an angle 0 (zero) with the reference direction then one can represent

its polarising properties by the Mueller matrix A(0). Similarly the cloud can be




represented by the matrix A (φ) with transmission coefficients k1 and k2. Now let

the light reaching the observer after it comes out of the cloud, be represented by the

Stokes coloumn matrix S = {I Q U V }. Therefore one may write

[S ] = [A (φ)][A(0)][S ] (7.9)

After the appropriate matrix multiplication one gets

I

Q

U

V

=14

I (k1 + k2)(k1 + k2) + I (k1 −k2)(k1 −k2)c2

I (k1 + k2)(k1 −k2)c2 + I (k1 −k2)(( k1 + k2)c22 + 2 s2

2k )

I (k1 + k2)(k1 −k2)s2 + I (k1 −k2)( k1 − k2)2c2s2

0

(7.10)

where k = k1k2. After simplication the above equation (7.10) reduces to

I

Q

U

V

=Ik 1k1(1 + f )

4

(1 + f ) + p(1 −f )c2

(1 −f )c2 + p((1 + f )c22 + 2 s2

2√f )

(1 −f )s2 + p(1 −√f )2c2s2

0

(7.11)

where f = k2/k 1 and f = k2/k

1.

Since the interstellar polarisation p = ( k1 −k2)/ (k1 + k2), one may also write

f = (1 − p)/ (1 + p) (7.12)




Figure 7.10: A model for cloud with the light from background star passing through it.



7.4.2:A model for the transmission coefficients of the cloud: 128

7.4.2 A model for the transmission coefficients of the cloud:

In general one may assume the cloud is spherical in shape, with radius R0. Now as

shown in Figure 7.10 , the background star is seen through the cloud, at a radial

distance r from the center of the cloud. Therefore, the starlight passes a distance

2h through the cloud, where h ∼ R20 −r 2. One may assume that the starlight

passes through ’2h’ number of layers through the cloud and the polarising effect of

each layer is equivalent to c (some arbitrary constant) times that of the IS medium,

where the later has transmission coefficients k1 and k2. This also amounts to the

assumption that the composition (characterised by k1 and k2) of the dusts in the

cloud and the IS medium are the same. However, within the cloud the grains may

have higher number density or may be better aligned, introducing a higher amount

of polarisation in the light from background stars. Grains may be also aligned in

a direction different from that in IS medium. This is the simplest possible model

which is considered for the present analysis. Now since there are ’2h’ number of

such layers, the equivalent transmission coefficients for the cloud would be ( k1)2hc

and (k2)2hc . In other words one writes k1 = ( k1)2hc and k2 = ( k2)2hc . The estimated

(or expected) value of polarisation pe present in the light coming out of the cloudcan be expressed as pe = √Q 2 + U 2

I .

Thus with the help of equation (7.11) one writes :

pe = ((1 −f )c2 + p((1 + f )c22 + 2 s2

2√f ))2 + ((1 −f )s2 + p(1 −√f )2c2s2)2

(1 + f ) + p(1 −f )c2(7.13)

At this stage one can consider two special cases when φ = 0 & 90 degrees and these

cases are represented by the following two equations:

pe(φ = 0) =(1 −f ) + p(1 + f )(1 + f ) + p(1 −f )

pe(φ = 90) = −(1 −f ) + p(1 + f )(1 + f ) − p(1 −f )

However in general when p 1, one can use the approximation

f = f 2h = ((1

− p)/ (1 + p))2h (1

−2hp)/ (1 + 2hp) and from equation (7.11) one

can write



7.4.3:Fitting the observed polarisation for radial distance from cloud centre 129

pe√ζ 1 + ζ 2

1 + 2hp2c2

where,

ζ 1 = (2 hpc2 + p(c22 + s2

2(1 −hp)(1 + 2 hp)/ (1 + hp))) 2,

ζ 2 = (2 hps 2 + p(1 −(1 −hp)(1 + 2 hp)/ (1 + hp))c2s2)2.

7.4.3 Fitting the observed polarisation for radial distance

from cloud centre

For all the eight clouds observed , the radial distances r (in arc sec) have beenestimated from the co-ordinates (RA and DEC) of each star available in Sen et al.

(2000). The polarisations observed for such eld stars in white light are plotted

against r , in Figures (7.11) and (7.12) . In some cases there is a trend (example

CB25, CB39), where as one moves away from the cloud center the polarisation

decreases and then attains a minimum value somewhere between 150-250 arc sec.

After that as one moves toward the periphery of the cloud, the polarisation value

increases and reaches the IS polarisation value as one nally moves out of the cloud.In order to nd some estimate for the interstellar polarisation for the nearby region of

the cloud, one can take a vectorial average of all the polarisation values (taking into

account the associated position angles in the measurements) that have been observed

for the outer most part of the cloud and assume that value to be representative of

the IS polarisation value (denoted by p, cf. Table 7.2 ). The same Table also lists

the distances corresponding to the outer most star, which is also assumed to be

roughly the dimension R0 of the cloud.The values of r and h assumed by us, in principle should be proportional to the

actual distances within the cloud. The quantity c in the expression h = c R2o −r 2

(as was introduced earlier in Section 7.4.2) can act as a proportionality constant to

normalise such distances. The value of c will be optimised later during model tting

the data.




Figure 7.11: Observed Polarisation versus radial distance plot for the clouds CB3,CB25, Cb39 and CB52.




Figure 7.12: Observed Polarisation versus radial distance plot for the clouds CB3,CB25, Cb39 and CB52. The curves joining the , represent our proposed model.




Table 7.2: The values of R0 (arc sec), interstellar polarisation p (in %), φ(in degrees), c, χ 2 are shown.

Cloud R0 p φ c χ 2

CB3 190 1.92 69 0.003 11

CB25 208 3.32 70 0.003 8

CB39 228 2.56 75 0.004 4

CB52 247 0.65 10 0.003 12CB54 379 0.40 10 0.002 23

CB58 279 1.90 60 0.002 62

CB62 207 0.40 0 0.002 8

CB246 191 1.84 60 0.004 13




After nding out r (and hence h) for each eld star, one estimates the polarisation

pe, using relation (7.13) and minimise the value of quantity χ 2 = ( pe− po)2

with c and φ as tting parameters (where po is the observed polarisation). While

minimising the value of χ 2, the data was not weighted with 1 / (e p)2, the justications

of which have been already discussed in Section 7.3.1. In Table 7.2 , one nds the

optimized values of c and φ, along with the corresponding minimised value of χ 2. In

this connection it may be mentioned that, while minimising the values of χ 2, it was

noticed that only at a unique set of values for ( c and φ), the minimum value for χ 2

can be obtained.

Figure 7.11 shows a plot of the polarisation values (po) observed for all the eld

stars in the clouds CB3, CB25 , CB39 and CB52, along with a curve representing

the polarisation ( pe) values as estimated using equation (7.13) and after best values

of c, φ have been obtained by χ 2 minimisation technique. Figure 7.12 represents

a similar plot for CB54, CB58 , CB62 and CB246.

From these two set of gures one nds that for some clouds like CB3, CB25 and

CB39 the polarisation value is relatively high at near the center region and then

reaches a minimum at a distance varying between 150-250 arc sec. After this it

increases again as one moves out of the cloud and reaches the region of IS medium.

At least for the clouds CB25 and CB39 this feature is more clearly seen. This

happens when the relative angle between the magnetic eld in cloud (related to the

direction of optic axis) and that of IS medium, φ is close to 90o.

For the other clouds CB52, CB54, CB58, CB62 and CB246 one can see this ideal

model does not t to the data. Thus one can rule out the possibility that these clouds

can be represented by a simple sphere containing an uniformly directed magnetic

eld, responsible for the alignment of grains. However, even an ideal cloud of above

type may not t to the observed data due to any (or all) of the following reasons :

1) There may be always some stars, which are foreground to the cloud. They will

however, exhibit very little polarisation, unless they are intrinsically polarised.

2) Some of the background stars, even may show high difference in polarisation from

the model curve, if the stars themselves are intrinsically polarised.

3) All the stars, background to the cloud are not placed at same distances behind



7.5: Conclusions 134

the cloud. As a result they are passing through different distances through the IS

medium and will have different values of IS polarisation in them.

4)If the shape of the cloud is different from an ideal sphere.

As at present it is not possible to distinguish the background stars from the fore-

ground ones, the ’goodness of t’ can not be improved any further.

The goodness of our t could have been also improved, if one could have measured

polarisation values sharply at a particular wavelength (say through narrow band

lters), rather than white light. This is because the polarisation produced by passage

through dichroic polarizer, as discussed above, has strong wavelength dependence

and stars are of various spectral types.

However, based on the present analysis one can not claim that a uniformly directed

magnetic eld (for that matter any aligning force) exists throughout the entire cloud

which is assumed to be spherical, with exceptions like in CB3, CB25 and CB39. In

clouds CB25 and CB39 ( and to some extent for CB3) the magnetic eld appears

to be quite uniform.

Further based on the present analysis one can also show that, the curve relating

pe with r can assume different shapes, according to different values of φ. So it is

not always necessary that, as one moves towards the centre of the cloud, the po-

larisation should also increase. Goodman et al. (1995), had questioned the validity

of background star polarimetry as a tool to study the cloud properties. The main

concern expressed by the authors was that as one moves towards the interior (cen-

ter) of the cloud the total extinction ( Av) increases, but the polarisation does not

increase as expected. However, with the help of present analysis one can show that,

the observed polarisation depends largely on the geometry of the magnetic eld (as

aligning force) within the cloud and as a result it does not always increase with Av.

7.5 ConclusionsThe polarisation observed for stars background to eight clouds (from Sen et al.

2000) and one from Kane et al. (1995) have been analysed and some of the major

conclusions are summarised below:

1. A histogram plot showing Rice corrected polarisation values against number of



7.5: Conclusions 135

stars, shows bimodal distribution with two peaks in polarisation values, for some of

the clouds. A possible interpretation in terms of a mixture of polarisation due to IS

medium and that due to cloud are discussed

2. A similar histogram plot with position angle ( θ) values, also shows some indica-

tions for bimodal distribution, which can be explained in terms of the inhomogenities

in magnetic eld geometry. However, the average direction of polarisation vector

and that of the interstellar magnetic eld seem to be the same.

3.The observed average polarisation in a cloud does not appear to be related to the

dust and gas temperatures as expected from Davis & Greenstein (1951) mechanism.

4.The observed average polarisation ( p) and turbulence (∆ V ) present in the cloud,

can be related by a line of best t ln ( p) = 1 .083 −0.2424∆V .

This nding bears importance as one can show that physical conditions within the

cloud can inuence the polarisation which one observes for stars background to the

cloud.

5. By assuming a given cloud to be a simple dichroic sphere, one can calculate the

expected polarisation values for stars at different projected distances from the cloud

center. This model can explain to a reasonable extent the spatial distribution of

observed polarisation in CB25 and CB39 (and to some extent CB3). But for other

clouds the model fails.

However, based on this model one can explain why polarisation always does not

increase with total extinction Av as one moves towards the center of the cloud.



References 136

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