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DEFENSE NUCLEAR AGENCY REACTION RATE HANDBOOK. SECOND EDITION. REVISION NUMBER 1
M. H. Bortner, et a 1
General Electric Company
Prepared for:
Defense Nuclear Agency
November 1972
L
DISTRIBUTED BY:
National Technical information Semes U. S. DEPARTMENT OF COMMERCE 5285 Port Rcyai Road, Springfield Va. 22151
_
i.y DNA 1948H (Formerly DASA 1948)
Revision No.]
DEFENSE NUCLEAR AGENCY
REACTION RATE HANDBOOK
SECOND EDITION REVISION NUMBER 1
Editors-in-Chief: Dr. M.H. Bortner
Dr. T. Baurer
NOVEMBER 1972
*
Project Officer: Dr. C.A. Blank
t>> APPROVED FOR PUBLIC RELEASE; DISTRIBUTION UNLIMITED
Organized by General Electric Space Sciences Laboratory For The Defense Nuclear Agency Under Contracts DASA 01-70-C-0082 and DASA 01-71-C-Oi45
This effort supported by Defense Nuclear Agency NWED Subtask Code HD028, Work Unit 11
Published by DASIAC DoD Nuclear Information and Analysis Center
General Electric, TEMPO Santc; Barbara, California 98102
NATIONAL TECHNICAI INFORMATION SERVICE
7
hV-?*¥*& MEMORANDUM
To: All Authorized Recipients of the DNA Reaction Rate Handbook (DNA 1948H)
From: The Editors
Enclosed herewith you will find a copy of Revision Number 1 to the Handbook. It comprises:
1. Revised interim version of Chapter 2, 2. Revised pages applicable to Appendices A, F, and G.
You shouid immediately substitute the enclosed items into your copy of the Handbook, discarding the corresponding pages which they re- place.
You should also enter on page iii in front of your Handbook the following information: Revision No. 1; Date of Issue- November 1972; Date of Receipt-whatever day you receive this; and sign your name in the last column.
Revision Number 2 is expected to be issued during the late spring or early summer of 1973. Thank you for your patience and cooperation.
CHAPTER 2
2 THE NATURAL ATMOSPHERE- ATMOSPHERIC STRUCTURE
K.S.W. Champion, Air Force Cambridge Research Laboratories (Latest Revision 16 March 1972)
N. B. : This chapter is not ready for publication, as of the latest re- vision dato, cited above. However, the. author has supplied selected reference data for the use of other authors elsewhere in the Handbook, and those authors therefore are enabled to cite Chapter 2 as the source of the information thus utilized. Chapter 2 will be prepared and distributed to authorized re- cipients of the Handbook at an early date. In the meantime, readers are encouraged to refer to the predecessor chapter by the same author in the First Edition of the Handbook, to other chapters in this Edition (numbers 4» 5, 13) in which data supplied by Dr. Champion are used as noted above, and to two papers* presented by Dr. Champion and his co-workers at the Fourteenth COS PAR Meeting, Seattle, Washington, June 1971. One of the two preprints referenced below is in- cluded herewith, in expanded form, as an interim version of Chapter 2.
-Champion, K. 5. W. , ' The Properties of the Neutral Atmosphere" , Paper R. 5; Champion, K.. S.W., and R. A. Schweinfurth, "The Mean COS PAR International Reference- Atmosphere", Paper F. 2, Fourteenth COSPAR Meeting, Seattle, Washington, June, 19? 1.
Revision No.I. November '972 2-1
DNA 1948H
THIS PAGE IS INTENTIONALLY LEFT BLANK.
2-2 Revision No.l. November i9?2
CHAPTER 2
v
THE MEAN COSPAR INTERNATIONAL REFERENCE ATMOSPHERE
K.S, W. Champion and R. A, Schweinfurth Air Force Cambridge Research Laboratories
Bedford, Massachusetts, U.S.A.
This contributed paper has been prepared for presentation at the Fourteenth COSPAR Meeting, June 1971 in Seattle. Paper F.2.
Revijiof» No.I, Novambar 1972 2-3
DNA 5948H
THE MEAN COSPAR INTERNATIONAL REFERENCE ATMOSPHERE
K. S. W. Champion and R. A, Schweinfurth Air Force Cambridge Research Laboratories
Bedford, Massachusetts, U.S.A.
1. INTRODUCTION
The new mean atmosphere has been developed for the altitude range 2 5 to 500 km. The basis of the reference atmosphere is as follows:
Between 25 and 7 5 km the model represents annual mean condi- tions for latitudes near 30°.
Between 120 and 500 km the model corresponds to diurnal, sea- sonal, and semiannual variation average conditions for a latitude near 30° and a solar flux F of 145 x 10"22 W/m2/Hz.
Between 75 and 120 km a model has been developed which pro- vides a smooth connection between the lower and upper sections of the meün atmosphere.
In addition, a basis is suggested for extending the model from 25 km to ground-level.
It should be noted that throughout the Mean Reference Atmosphere the same formula (appropriate to a latitude of 30°) lias been used for the acceleration due to gravity.
This atmosphere contains temperature, density, pressure, densi- ty and pressure scale heights, mean molecular weight, densities of major constituents, and total number densities.
The reasons for providing a Mean Reference Atmosphere are two- fold:
(1) For many computations it is unnecessary to include a variety of atmospheric conditions and it is sufficient and economical to use a single typical model oi the atmosphere.
2-4 Revision No.I, November 1972
CHAPTER 2
•*. .*
2) The respective low and high altitude models of the Reference Atmospheres are functions of different parameters and do not match at 110 km. Thus, if computations are to span this al- titude it will, in general, be most satisfactory to use the mean model.
= N
•« f
2. MODEL BETWEEN 25 AND 75 km
The data used to develop this model were the annual mean pres- sure value at 25 km at 30 latitude and the annual mean temperature values at 30 latitude at 5 km intervals starting at 25 km derived from Groves [lj. The actual values are as follows:
3 •> Pressure at 25 km: 2.483 x 10 newtons/m*"
Altitude (km) 2 5 30 3 5 40 45 50
Temperature (K) 221.7 230.7 241.5 2 55.3 267.7 271.6
Altitude (km) 55 60 65 70 75
Temperature (K) 263.9 249.3 232.7 2:6,2 205.0
Starting at 2 5 km the atmospheric properties were computed using the following equations. Simpson's Rule was used to integrate numeri- cally the pressure equation:
P = Pj exP
M
R gdz/T M
T U)
where: p
P
M(
R
g
T
T
M
M
pressure at reference altitude z.
pressure at altitude z
sea level value of mean molecular weight = 28.96
universal gas constant = 8. 31432 x 10 ergs K grnole
acceleration due to gravity
molecular- scale temperature
M
lfT • (2>
Revision No.I, November 19?? 2-5
DNA 1948H
where M = mean molecular weight
T = kinetic temperature.
The total density was calculated from the relation;
pM o RT RT
(3 M
The pressure scale height was calculated from:
RT. Hp
RT M
Mg M g
As the aim of the computations was to derive a model for the al- titude region 25 to 500 km 'using a single expression for the accelera- tion due to gravity the expressions used respectively for the low and high altitude models were investigated. Unfortunately, neither for- mula was adequate. The formula used by Groves was the same as in CIRA 1965 and was sufficient in all respects except that its accuracy at high altitudes was not acceptable. The error was 1 in 10 at 200 km, 4 in 10 at 300 km, and increased rapidly with altitude. On the other hand, the expression used by Jacchia [2 j is valid only for a latitude near 45° (45°32'33"). The problem was solved by adding another term to the expression used in CIRA 1965. The basic ex- pression due to Lambert L 3 J includes dependence on latitude 0:
= e - (3.085462 x 10 4- 2. 27 x 10~9 cos20)z
+ (7. 2 54 x 10
- (1.517 x 10
"13 + 1. 0 x 10"15 cos20)z2
+ b x 10"^ cos20)z"' m/sec' 5)
where z is in meters.
The form applicable to 30' latitude is
g = 9. 79324 - 3. 086597 x 10~6 z + 7. 259 x 10"i3 zZ
-19 3 , 2 - 1. 520 >: 10 z m/sec . 6)
2-6 Revision No.I, November 1972
CHAPTER 2
*% .•>' 3. MODEL BETWEEN 75 AND 120 km
The model in this region has to provide a transition between the low altitude model based on Groves' data [l] and Jacchia's high al- titude models [2 J. Jacchia1 s models start at 90 km and Groves' models extt nd to 110 km and they are not only different but they are functions of different parameters. Obviously a compromise must be devised.
As a starting point a temperature profile had to be chosen. As inputs for this it is interesting to compare the values from several models given below:
Temperature (TM, K)
Altitude USStdAtm rTD . 10/r r- . -<- T- u- +
„ .«,„ CIRA 19ö3 Graves* Jacchia (km) 1962
80 180.65 186.0 197.3 -
90 180.65 186, 0 189. 0 183. 8
100 210.65 213.0 215. 1 203. 5
110 260. 5 263.0 284. 0 265. 5
120 360.65 380.7 _ 380.6
^Average annual values for 30" latitude converted from kinetic temperatures using the values of M in reference [ 1 ].
+ Average values for 45° latitude from model with 1000 K exospheric temperature using the values of M in reference |_2j to convert the Kinetic temperatures.
Two points should be noted. One is that Groves' t *;«ii.. L:_L — 4i. .. -.i - i • .i ' ' ui*uy li-igii^j. mau mal AH UtllCI' IIIUUKlh.
mperature at The second
is the differences between the temperatures of the Groves and Jacchia models. A further constraint on the temperature profile used in this altitude region is that it must yield a specified density value at 120 km. The values determined for the molecular-scale temperature (TV») are:
Altitude (km) 80 90 100 110 120
Temperature (T K) 195.0 183; 8 203.5 265.5 380.6
The adjustments in the temperature profile were made between 75 and 90 km.
Reyition No.I, Novembflr !972 2-7
DNA 1948H
Composition was calculated for this region by J. D. George using the techniques of George, Zimmerman, and Keneshea [4J, which in- clude the effects of chemistry and atmospheric dynamics.
The equacions used are a system of mass and momentum conser- vation equations given below for the i'th species:
on- l
du. i
or
F- - n-R. - i i l
&(n.u.) dcp.
Sz öz
/ on. -kT / _1_ _* + _JL Ü m, \ n. öz T dz 1 \ i H.
- IN-JC.u. 2 i i 81
wh ere:
u
t
7.
F. 1
n.R. l i
k
m.
H. i
n.[N. JC. l £ i
= the concentration of the i'th species
= the mean velocity of the i'th species
= V. + ü i
= the diffusion velocity of the i'th species
= the mean mass velocity
= time
= altitude
= chemical formation rate of the i'th species
= chemical removal rate of the i'th species
- Boltzmann constant
- mass of the i'th species
- scale height of the i'th species
is proportional to the frequency of collisions between N2 and the i'th opecies.
tp- is the turbulent mixing flux for the i'th species given by:
. "ni I 1 ST 1
m (9)
2-8 Rcviiiun No.I, Novimbir «972
IB 'y CHAPTER 2
where K* is the turbulent diffusion coefficient and H is the scale c m height of a species with the mean mass.
At the lower boundary at 75 km -NU, O.., Ar, and He were assumed to have the same mixing ratio ?.s at ground level taken from the U. S. Standard Atmosphere, 1962. At this boundary the species Oanl O3 were chemically determined by:
on. - = F- - n.R. t * l 1
(10)
Although not printed in the tables the following species were in- cluded in the computations and their densities determined: H2O (ground level mixing ratio at 75 km), OH, H, H2, HO^, and H-»0?
(chemically determined at 75 km).
The mean velocity (u^) was assumed to be zero for ail species at the upper boundary at 120 km. The turbulent flux for all species is also zero at that altitude since the assumed turbulent diffusion coef- ficient Kt is zero above the turbopause at 100 km. The concentra- tions of Np, O-, O, Ar, and He were fixed at the upper boundary at the values for the high altitude portion of the model. The remaining species were assumed to be in diffusive equilibrium.
Since a diurnally varying solar flux was used with equations (7), (8), and (9) periodic solutions are obtained. The solution was con- tinued for 32 problem days for a latitude of 30° N using a fixed de- clination angle (0 or equinox) resulting in a periodically varying zenith angle. The choice of 32 days wa1; arbitrary but did result in adequate accuracy. The variation in the densities of ail species was less than one part per thousand from no.m of day 3 1 to noon of day .32. The mean profiles presented here were obtained by averaging over the final 24 hours at 15-minute intervals. One of the constraints of the solution was to maintain a fixed molecular scaie temperature profile. The kinetic temperature profile was derived using the solu- tion mean molecular weight. The kinetic temperatures were used to compute the M? concentrations in the diffusive equilibrium region from 101 to 120 km. A transiMon from diffusive equilibrium at 101 km to mixing at 99 km was made nsin»? a cubic to represent loginCN?], Below 99 km, the mixing region for No» the initial I r,j profile was not changed.
Ravision No.I, Novoinbe? 1972 2-9
W?*W'?WWV«'IW•«*«¥»I>•»*'W«HTOJ^
DNA I948H
In performing the computations the variation with temperature of the reaction rate constants R- was included, as well as the effects of absorption by the O^ and O-, column densities un the dissociation rates by sola.r ultraviolet radiation. The finite difference analogues used are essentially those given by Shimazaki [5] with modifications as cited by George, Zimmerman, and Keneshea [4]. However, the technique used is modified in that the equations are treated as fully implicit throughout the solution. This approach should preserve the conservation cf atoms within the solution altitude region (75 to 120 km) with the exception cf the loss of atoms through the lower boun- dary.
4. MODEL ABOVE 120 km
The exospheric temperature was calculated to correspond to average diurnal, seasonal., semi-annual, and geomagnetic conditions for 30° latitude and a solar flux of 145 x 10_2Z W/m2/Hz. The re- sultant exospheric temperature is 1000 K-
Jacchia's models were recomputed from 90 km upwards usir^ the expression ior g given in equation (6). This results in a cha ige in the total density and number densities of the constituents at higher altitudes. The densities were then changed (at all altitudes) so that at 120 km they matched the density computed for the intermediate altitude model. These densities are very close to those of the 1000 K Jacchia model at 120 km as shown immediately below, but are slight- ly different at other altitudes.
-3. Altitude (km) Temp (K) Log [N2 ](m""3) Log [023(m"-)
120 334. 5 17.5789 16.7338
-3, Log L O J (m " -) Log [ Ar „»{m~ ) Log [He } (m
17.1532 i5.1~32 13.5376
M
2 5. 45
Density (kgm )
2.438 x 10"
Above the turbopause (assumed to be at 100 km) the number den- sities of each individual species n- were computed by integrating the equation for diffusive equilibrium:
2-10 RavUion No.I. November 1972
CHAPTER 2
tin, M.g —- = - -~dz - (1 + Oi.) —. , (11
n. RT i T i
where 0!- is the thermal diffusion coefficient taken to be -0. 38 for helium and zero for other constituents.
5. MEAN REFERENCE ATMOSPHERE
The properties of the Mean Reference Atmosphere are presented in Tables 1-4. Table 1 contains values of molecular scale tempera- ture, density, log density, pressure, log pressure, number density, pressure scc-le height, and acceleration due to gravity over the alti- tude range 25 to 120 km,* Table 2 contains values of kinetic tempera- ture, mean molecular weight, and log number densities of Nj», O2, O, Ar, He, and O3 over the altitude range 75 to 120 km. Densities of O and 0> are not presented below 80 km because at these altitudes their diurnal variation is so large that average values would have little significance. The O3 densities presented are for noon. In Table 3 are given molecular scale temperature, density, log density, pressure, log pressure, pressure scale height, and acceleration due to gravity for the altitude range 120 to 500 kin. Table 4 contains the corresponding values of kinetic temperature, mean molecular weight, number density, and log number densities cf N£, O?, O, Ar, and He for the altitudes 120 to 500 km.
The properties of the Mean Reference Atmosphere are illustrated in Figures i-7. Figure 1 shows the pressure scale height as a func- tion of altitude. Figure 2 shows the kinetic temperature (T) and the molecular-scale temperature (T^j). Figure 3 contains the kinetic
*Th.fi Mean CIR.A ha.s been dove?or"?d ^or th<? z*]titnAe' ranae* ?.^ to ^00 km. At 2 5 km the Mean CIRA values are almost identical with those of the US Standard Atmosphere Supplements, 1966 midlatitude spring/fall model. Thus the values in Table 1 can be extended to ground level by using the numbers in Table 5. 1, page 110 of the Supplements. If an exact match is required for a given parameter, e. g. , temperature, density, or pressure, then the Mean CIRA 25- km value can be matched to the Supplement value slightly above 2 5 km (25. 15 km for temperature) and then the Supplement altitude values scaled accordingly. Physically this can be justified because different g values were used in developing the two models (45 N and 30 N values for the Supplement and the Mean CIRA, respectively).
9 " Revision No.I. November 1972 *•
W<jufc»W PWIWWI!£-' W5WW0BBWIJPHI •w. i vi»L•«?Hff«r'vw:P mm '.»rawwww.^wwiswarF -»MW" nif.Mm«v<'>W!
DNA 1948H
temperature of the mean atmosphere plus curves indicating low ex- treme and high extreme temperatures whose frequency of occurrence is one per cent or less. The extreme curves attain exospheric tem- peratures of 550 and 1900 K, respectively. The pressure curve for the Mean Atmosphere is shown in Figure 4. Low extreme, high ex- treme and mean density values are plotted in Figure 5. Above 180 km. these curve« correspond to the temperature profiles in Figure 3. The mean molecular weights for the mean atmosphere are plotted in Figure 6. The corresponding number densities of N^» O-., O, O-j, Ar, He, and H are shown in Figure 7.
To illustrate very large seasonal variations, Figure 8 contains the mean June-Jaly temperature profile for 80° N and Figure 9 the mean December-January temperature profile for the same location. These profiles are based primarily on data from Heiss Island and are from Reference [6]. At 50 km the temperatures range from 279 K in sum- mer to 247 K in winter, compared with the mean reference value of 271. 6 K. At 80 km they range from 177 K in summer to 218 K in winter, compared with the reference value of 195 K.
Figure 10 contains the mean CIRA temperatures, median warm temperatures and those exceeded 10% and 1% of the time and, simi- larly, median cold temperatures and those above which 90% and 99%, respectively, of the temperatures lie. The extreme temperature profiles are a revised version of those in Reference i_7~!. The cor- responding density curves are shown in Figure 11. In general, the mean atmosphere values are in excellent agreement with the other curves.
6. REFERENCES
[1J G. V. Groves, Seasonal and latitudinal models of atmospheric f nperature, pressure and density, 25 to 100 km, AFCRL-70- 0261 (1970).
[2] L.G. Jacchia, Revised static models of the thermosphere and exosphere with empirical temperature profiles, Smith son. Astrophys, Obs. Spec. Report 3 32 (1971).
[3] W. D. Lambert, Acceleration of gravity in the free air, in Smithsonian Meteorological Tables, r>ixth edition, Washington (1951) p. 490.
2-12 Revision No.i, November 1972
iBW»WMMViiff»iH,qp^fli^iii^ vB^^^^^pmw^^'t^wvvsif^!^vr!m^r>«<a^^^9ff
CHAPTER 2
[4] J. O. George, S. P. Zimmerman and T. J. Keneshea, The lati- tudinal variation of major and minor neutral species in the up- per atmosphere, to be published in Space Research XII, Berlin (1972).
[5] T. S. Shimazaki, J. Atmos. Terr. PhyS. 29, 723(1967).
[6] Supplements to the Project cf ttis International Standard Atmos- phere Model, ISO/TC-20/SC-6 (Secretariat-30) (1970).
1.7] A. E. Cole, in: Space Research XI, Akademie-Verlag, Berlin (1971) p. 813.
Revisio«' No.i, Novcmbor 1972 2-13
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CHAPTER 2
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2-26 Rtvltion No,I, Novambtr 19/2
BWjISHWBWWBlHBreWWWTg1^^ WW^'-«»«^^^'****'^^
CHAPTER 2
500
400-
300-
a
200^-
0 10 20 30 40 50 60 70
PRESSURE SCALE HEIGHT (km)
Figure 1. Pressure scale heights of the mean CIRA atmosphere
500
400
g 300
IOC
400 800 JL I L
1200 TEMPERATURE ( K)
1600 2000
Figure 2. Kinetic temperatures (T) and molecular-scale temperatures (Tu) of the mean atmosphere.
Rtvition No.I, Nov«mbtr 1972 2-27
TOrTW£^«»w>"HT^--^F7^>v'•j"iw*i^T;•-«-w^T^
DNA 1948H
500
400 r
e 300 -
< 200 -
100 -
LOW MEAN HIGH EXTREME CIRA EXTREME
T ( j j 1 r
400 800 1200 1600 2000
TEMPERATURE ( K)
Figure 3. Mean CIRA temperatures and low extreme and high extreme temperatures.
500 njmr rrrpirTTTTBl rrf^ir^TTpiriTrprTTrpij i i «IIIIK—rTTfmr
UjIlULl iilftii LliiUli Liililili I !JuiiC.l Uiiit J I JjJlLIIIluli lilllKI l.liM J.liliiB 10" lö5 iO" 10' 10°
PRESSURE (newtons/m )
Figure 4. Pressure curve of the mean atmosphere, from 25 to 500 km
2-28 Revision No.I. November 1972
«PS ^SV|I^P!!WP>9ffW^V!lf^!WH!^H^EPl|IRRJ!Mi 'iPP H'ÄW p,|,^WAV^',^^W^fe/w<T*^'fl•W^I,"?, psr«».:*^MiHWtjfflHUJj^wyiatSP HP»
CHAPTER 2
LOW MEAN HIGH
500
400
EXTREME CIRA EXTREME
E 300 -
ROO
100 -
iö !0 DENSITY Ug/m»)
Figure 5. Mean CIRA densities ond curves of extreme densities
5C0
400 -
§300 -
< 200 h
100 -
14 16 18 20 22 24 26 28 30
MEAN MOLECULAR WEIGHT
Figure 6. Mean molecular weights of Mean CIRA atmosphere
Revision Nc.i, November 1972 2 »29
lUJiftWVfminWK!"1 IWWWl^p^lWM.' '^iwrvr^mr'^^^iera^r^^t'r^^'^^^f
DNA 1948H
500-
400
300
200
100
_l ^ T 1 _j. I i ! I
\' \ I
J L 20 10° 10" I0,w 10" 10" I0'e 10'" 10
NUMBER DENSITY (M*3)
Figure 7. Total number densities and densities of N2/ O2/ O, Cg, Ar, He, and !J,
80
70
60
50
40
30
20
10
/
/
i \. , ... .
\
"^ !!lSa*
180 200 220 240 260 280 TEMPERATURE (SO
Figure 8, Mean June-July temperature profile for 80° N
2-30 Rjviiior. No.I, Novsmbm !S72
Wtmmm*!MVm,W*»»»wr-M-**'am^w*r'~»~-*.T~>,~*.-~~,-~,-*,,. ._
ft 4 I
CHAPTER 2
80
70
60
I 50 a
< 40
30
20
10
a
i I
,
\
L
j j
V
... >. . _ ._ L 180 200 220 240 260 280
TEMPERATURE (K)
Figure 9. Mean December-January temperature profile for 80°N.
90
80
I70
% C0
COLO TEMPERATURES M~EÄN~T
L ,,90% /MtD'AN ClRA,
99% \ /
WARM TEMPERATURES
50
40
30 r
130 150 170 190 210 230 250 270 290
TEMPERATURE T„ ( K)
Figure 10. Mean CIRA temperatures, temperatures which are exceeded 50, 10, and 1% of the time during warmest months and temperatures exceeded 50, 90, and 99% of the time during coldest months at latitudes between 0° and 80° N.
Revision No.I. Novtmbtr 1972 2-31
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APPENDIX A
B Designation in Figure 16-2, for work of bardsley, Reference (cont'd) 16-28 (16).
Power of the pre-exponential thermal dependence, a charac- teristic term oi" tlie rate-constant function (19).
Magnetic field strength (21).
Indexing use: target species (15).
3H
Bo
B&T
Bo
b;
N2
buoy
b,
C
Designation for Birge-Hopfield system (9).
Comparison real function plotted in Figure 21-2, from Reference 21-2, assuming j=0 and V{z)-V (21).
Designation in Figure 20-6, for work of Bauer and Tsang, Reference 20-143 (20).
Real function plotted in Figure 21-2, from Equation 21-5 (21).
Power of the pre-exponential thermal dependence, a charac teristic term of the rate-constant function (6, 16, 19, 24).
Parameter defined in Equation 15-10 (15).
Impact parameter (15).
Indexing uses: bound state of species (8). trajectory point (15). impact parameter (15). colliding species in the Firsov model (15). magnetic field (21).
Interaction or capture radius (15).
Capture probability (15).
Indexing use only; buoyancy subrange (3).
Cut-off radius (15).
Designation for unspecified chemical species (6, 19, 20).
Linear slope in a Boltzmann system (6).
Designation in Table 9-5, for chemical association process (9).
A-3 Reviiion Not, November J972
WSKWS^-JPOTWJ*.^ *ym»Bin»gPttW*BgWMW^^
DNA 1948H
C Designation in Table 15-2, for fast-particle detection (15).
*°°n Constant SB 3. 49 in the Thomas theory (15).
Least-squares fit constant (16).
C. Collision proportionality constant for species "i" (2).
$ (X) Integral function of X used in Equation 21-5 and explained and tabulated in Reference 21-28 (21).
c Speed of sound (3).
Speed of light {4, 7, 11),
Activation temperature of chemical reaction, a characteris tic term of the rate-constant function (6, 19, 24).
Indexing uses: chemical change (3). chemical energy (3). cyclotron(7). cone (7). collisional (20).
c Mean thermal speed (3).
c. Mean thermal speed of species "j" (3).
cQ Speed of sound in unperturbed medium (3).
col Indexing use only; column (11).
crit Indexing use only; critical value (3).
c Specific heat at constant volume per unit mass (3). v
IT* 'I x^'
D Effective diffusion coefficient (3).
Dissociation energy (4).
Distance from nuclear burst measured along surface of earth (5).
Designation for unspecified chemical species (6).
Designation in Table 15-2, for slow-particle detection (15).
Least-squares fit constant (16).
A-4 Revinion No.), November 1972
^?*>W,*,«?"PPPGS*3»?^^ ißfiwiwmtmmmwmmmww*m*1': IBP!*
APPENDIX A
E XA
E.
eddy
eff
ex
F
F
F!
Fi
Activation energy for collisional excitation (X-»A) reaction (20).
s MR (E'/13»f») , in the rne hod of Fleischmann, Dehmel, and Lee (15).
Kinetic energy of incident ion before collision (15).
Kinetic energy of incident ion after collision (15).
Ionic or electronic charge (7, 11, 15t 21).
Designation in Table 9-5, for photoelectron process (9).
Indexing uses: energy equation (3). electron (4, 5, 7, 8, 11, 16, 20, 21, 22, 24). electronic transition (11). bound electron (15), electron acting as third body (16).
Indexing use only; eddy (3).
Indexing use only; effective (9, 15)..
Indexing use only; excitation (4, 11).
St ).ar flux at 10. 7-cm wavelength (5).
Designation in Table 9-5, for fluorescence process (9).
Free energy (10).
Fraction of optically active molecules under irradiation, vvhi are radiatively excited per second (11).
Designation on Page 18A-8, of work of Ferguson, from Reference 18A-9 (18A).
Designation on Page 18A-9, of work of Fehsenfeid et al, from Reference 18A-40 (18A).
Mean ?olar flux (2).
Total external force per unit mass (3).
Miscellaneous external forces acting on atmosphere (3).
Extern&l force per unit mass on species ''a" (3).
Chemical formation rate of species "i" (2).
Revision No.I, November 1972 A-7
iswBapSPWtfWiw^iiw^^
DNA 1948H
F(k) Turbulent power spectrum, in wavenumber space (3).
F(k)., F(k) in the inertial subrange, according to Kolmogoroff s Law (3).
f Oscillator strength or "f-number" of transition (11).
Range of reciprocal electron densities over which a linear variation with time is obtained, to within one percent (16).
Indexing uses: fluorescence (11). final (11).
f Resonant frequency (7).
f Fraction of collisions having relative velocities between v v / c
and v+ dv (o).
f(X)
G
Fractional atmospheric concentration of species "X" (4).
Electron energy distribution function (21),
Fractional energy loss per collision (21).
G(i, t) Prooability for separation distance »"i" between two parti- cles (3).
GS Designation in Figure 16-2, of work of Gunton and Shaw, from Reference 16-7 (16).
g Gravitational acceleration (2, 4).
Production rate factor (9).
Statistical weight (11).
Indexing use: gas-kinetic (21).
g Gravitational force per unit mass (3).
gas Indexing use only; gas-kinetic (16).
g- Statistical weight of ionic ground state (II).
g , Statistical weight of a recombining level "n/" (11).
A-8 Revision No.l, November 1972
.-,..- ^ - j^^f^^l^^wpgtWHTO^^ WW5S»W7W^1^^ *
APPENDIX A
g(X)
g(y)
H
Ha
HCE
H:
m H.
KP H(X)
*
n.. ii
h'j
Statistical weight of a recombining level in a hydrogenic species (11).
Electronic statistical weight of specie "X;' (4),
r 0. 1 1 Firsov model parameter =Jy - 1| (15).
Atmospheric scale height (3).
Magnetic field (7).
Scale height of atomic oxygen (9).
Enthalpy (10, 17. 19).
Total Hamiltonian (15).
Designation in Figure 16-1, of work of Hagen, from Refer- ence 16-22 (16).
Designation on Page 18A-9, of work of Howard et ai, from Reference 18A-12 (18A).
Scale height (20).
Indexing use: hydrogen atom (15).
Designation in Figure 16-1, of work of Hackarn, from Reference 16-19 (16).
Designation for Handbook Committee PDstirnate (24).
Scale height of species "i" (2).
Scale height of species having mean mass (2).
Pressure scale height (2).
Scale height of species "X" (4).
Planck constant (3, 4, 6, 7, 11, 17, 19, 20, 2,4).
Altitude (4, 5).
Indexing use: altitude (4).
Modified Planck constant, h/Zv{ll, 15).
2 (0-, V, 0.) i b l
(fl., V 0.) i a j
15).
pBvisioii No.I, Novomber 1972 A-9
DNA 1948H
h - (0 Vb0.) J \ (15).
hy - <*j, Va0jt
h. " A measure of chemical effect in turbulence, from Equation 3 3-67a (3),
h Turbopause altitude (4).
Indexing use: turbopause altitude (4).
horiz Indexing use. only; horizontal (3).
h Quenching height (9).
I lonization potential (4, 15).
Photon flux after transmission (7).
Intensity of indicated radiation (9).
Geomagnetic dip angle (9).
Designation in Table 9-5, of ionic reaction process (9).
It Line-of-sight column emission rate = line integral of I , "(11).
ICR Designation for Ion Cyclotron Resonance (7).
IGY Designation for International Geophysical Year (9).
I„ lonization potential (13. 6 eV) of ground-state hydrogen
Im Designation for imaginary portion of function (21).
ImAKi Imaginary portion of AKi , in the low-frequency limit (21).
I Photon flux before transmission (7).
IQ(X) Incident light intensity (12).
IP lonization potential (i8A).
IR Infrared.
A-10 Revision No.], November 1972
T—f fif—"-w-r—mmi.mj u. * PPn^ppmP9P9PPPS!iP
APPENDIX A
Kt
K'
K
K
K
K
01
10
k
k.
3n
kin
k.(z] J
M
kn
Turbulent diffusion coefficient (2).
Collisional rate (11).
Collisional excitation rate (11).
Collisional deexcitation rate (11).
Thermal conductivity coefficient (3).
Degree of ionization of plasma (3).
Wavenumber (3).
Boltzmann constant (2, 4, 11, 20, 21).
Rate constant or rate- constant function, of chemical reaction, in the forward direction as written (6, 11, 18A, 19, 20, 24).
Total absorption coefficient (7).
Rate coefficient of ion-molecule reaction (8).
Total three-body recombination rate coefficient (16).
Indexing use: kinetic (4).
Wavenumber vector (3).
Upper limit of wavenumber for buoyancy subrange (3).
Photoionization coefficient (7).
Rate constant for inelastic scattering from species "i" (20).
Rate coefficient for Thomson recombination, three-body i__ 1 l 1 _ _*__ u .'i : _ .. i -..-:..:..- .• _ .. .. A. • . . - : - . iivuii ui - uiviCVUtG ~ aiauin^cu, uuoi-i yc"iuii"iicganvc"iuii
recombination (16).
Indexing use only; kinetic (11).
First-order rate constant for photoionization of species "j", at altitude "s" (13).
Rate constant for quenching reaction where "M" is the quenchant (20).
Reactive collision frequency (20).
Rtvitror. No.I, Novsmbtr 1972 A-13
aw'WWlW'y'WlWP**'*'»*'1.'mmt umnwr^ »«r^wwwww»!^^ w^-w^^mwm^^
DNA 1948H
k(NO ) Rate coefficient for NO+ production {13).
k o
T
k{v)
= 2ir/L0 (3).
k Rate constant for reverse reaction (18A).
Rate constant for a system having Maxwellian distribution (6, 14).
Absorption coefficient (12).
Rate constant for formation of vibrationally excited specie: in level 'V (11).
Wavenumber directional components (3).
= Zff/L,^ (ClJvy)l/4 (3).
Rate constant for deactivation of first vibrational level (20),
Three-body recombination rate coefficient with electron as third body (16).
Three-body recombination rate coefficient with neutral species as third body (16).
Three-body recombination rate coefficient (16).
Rate constant at 300 K (24).
k' Rate constant or rate-constant function of chemical reac- tion, in tho reverse direction as written (6).
h Boltzmann constant (3, 6).
L Designation for Lyman radiation (5).
Optical pafhlength (13).
TO
•3e
•3n
\3r
k 300
LBH Designation for Lyman- Birge-Hopfield system (9).
A-14 Revision Na.J, Novomber j97?
».T^,,,u-rr^w,1i5-wn.^iB-*.•.>•^rr,v^-^-i.m-^^TJ--,->T-.-^'r ----^»—.-. .-:.^.,.-rrm)r-*rav~**pnK7T.-.w-"-r~- '•^.-»T--^«^»r':"^r-^i--N»Mfw-^B|.^-vfii-w--»r.?-v.-i»W7Tl''T' •' '"^W^ T*CTB» 7»frrsr^w»»^«TW^T!51T^W^?'r^ww^WT/w»IT^^»ÄKp
hj«>
L. J
-1
Lj(c)
Lo
LT
LTE
Ly
Me)
L 'y
I. 2r
L 3r
m
M
APPENDIX A
Inelastic cross-section for low-energy electron in gas (21),
Rate of process "j" leading to electron loss (16).
A measure of the effect of wind shear in turbulence, in Equation 3-67b (3).
Energy loss function for the jth vibrational level (21).
Length scale of large (turbulent) disturbances (3).
Designation in Figure 16-2, of work of Lin and Teare, from Reference 16-27 (16).
Designation for Local Thermodynamic Equilibrium (4, 11).
Designation for Lyman radiation (12).
Energy loss function (21).
Length scale of the smallest of eddies (3).
Rate of electron loss via two-body electron-ion recombina- tion (16).
Rate of electron loss via three-body electron-ion recom- bination (16).
Distance (3).
Charged rearrangement rate constant for negative ions (9).
Light path (12).
Gas-kinetic mean free path (3).
Mean molecular weight (2),
Cram molecular weight (3).
Reduced molecular weight (6).
Designation for third body or collisionaJ partner (6, 16, 17, 18A, 19, 20, 24).
Reduced mass of ion-molecule reaction pair (8).
Revision No. 1, November 197? A-15
^•~•^mmmmm*mmmmmmm*****<•m'm'm**^^^^'^^^^*mm mmm^^fS ysrcajii'iww« «Bg^B^Wig
i *?!«IK-f '*'*.' -—•-< -•*
DNA 1948H
M (cont'd)
MB
Me
M.
M o
M(X)
m
m
in av
max
Projectile mass, in the method of Fleischmann, Dehmel, and Lee (15).
Designation for unspecified chemical species (17, 18A, 20).
Number of density of collision partner (20).
Mass number (21).
Indexing use: molecular-scale (2).
Designation in Figures 16-1 and 16-3, of work of Mehr and Biondi, from Reference 16-21 (16).
Designation for unspecified metallic species (11).
Molecular weight of species *'i" (2).
Mass number for an ionic species (21).
Reduced mass of ion + neutral pair (21).
Sea-level mean atmospheric molecular weight = 28. 96 (2).
Mass of species "X" (4).
Mean mass of an "air molecule" (3).
Unspecified function of altitude, time of day, and sunspot cycle (5).
Ionic mass (7, 15).
Concentratioxi of attaching neutral species (9).
Mass of electron (21).
Indexing uses: mean-mass (2). equation of motion (3). combining proportions (6). molecular (9). momentum-^ansfer (11, 21). number of electrons stripped (15).
Molecular mass of species "a" (3).
Mass of average "air molecule" (3).
Indexing use only; maxi3Tmm (11).
A-16 R »vision No.I, Nov«mbtr 1972
IPP9|IOT)fflPN|CII|5KPIPPRil9ipnRPIl|^PI
APPENDIX A
rn
TCi. 1
m
m.n
mol
m.
N
N i col
NED
N ex
N. l
[N.] J
N+
N
N mi
Mass of electron (4, 11).
Mass of bound electron on target atom (15).
Mass of species "i" (2).
Molecular mass of species "j" (3),
Indexing use only; mutual neutralization (16).
Indexing use only; molecular (3).
Mass of incident ion (15).
Designation for north latitude (2).
Number of observations (3).
Brunt-Vaisälä frequency (3).
Electron concentration (9).
Number of collisions per second per molecule at altitude (11).
Total number of optically active molecules under irradiation (11
Designation for unspecified chemical species (16).
Molecular density (21).
Indexing use: neutral product (12).
Column density of molecules under radiative excitation (11).
Designation for No Experimental Data (24).
Total number of optically active molecules under irradia- tion which become excited (11).
Positive-ion density (21).
Concentration of species '"j" (13).
Positive-ion concentration (9).
Density of atomic ions (9).
Density of molecular ions (9).
Roviiion No.I, Novombor I9?2 A-17
g^^-igTiq^^WCT^Kin»;!^.^^^*-^^
DNA 1948H
N Negative-ion concentration (9).
n Species concentration (3).
Gas density (7).
Concentration of detaching neutral species (9).
Level of hydrogenic species into which recombination is taking place (11).
Density of absorbing gas (12).
« -b for certain recombination reactions (19).
Electron density (21).
Indexing uses: combining proportions (5, 6, 16, 17, 21, 24). level of hydrogenic species (11). final charge on initially neutral target species (15] neutral species acting as third body (16). electron noise (21).
n Number density of target species (15).
n Electron density (4, 5, 7, 8, 11, 16, 22). e
(n (tn Space-averaged electron density at time "t" (16).
(n (On Space-averaged electron density at zero time (16).
n (co) Stationary electron density long after ionizing source is e ' turned on (16).
n Number of electrons effectively available for ionization in et f the outer shell of projectile species, in the method of
Fleischmann, Dehmel, and Lee (15).
n. Number density of species "i" (2, 20).
Ion density (11).
n.R. Chemical removal rate of species "i'* (2). j. l
n. Number density of species "j" (3).
n. Fluctuation of n. (3). J J
A-18 R «vision No I, November 1972
w**m*rr*m»*i Km^wfmw!^^mvm''m^^^m^mm^i^ WP^WK
APPENDIX A
nj
nit
n N-
n
n
n tot
n(X)
n
n.
n,
Mean value of n- (3).
A particular level into which radiative recombination is taking place (11).
Indexing use: level into which radiative recombination is taking place (11).
N^ species density (24).
Loschmidt number (7, 12).
Density of stabilizing agent (16).
Total species density (4).
Species density of "X" (4).
Vertical distribution of atomic-oxygen concentration (3).
Vertical distribution of molecular-oxygen concentration (3|
Positive-ion density (16).
Negative-ion density (16).
Indexing uses: sea-level (2). unperturbed-medium (3). reference (3). turbopause (4). pre-magnetic storm (5). pre-transmission (7). resonant (7). Loschmidt (7, 12), standard-state (10). band1- origin (11). atomic species (11). incidence (12). impact, in the Firsov model (15). Bohr (15, 21), collision-free (20). free-space (21). energy-independent (21). pre-integration (21).
Revision No.l, No«»mbe- 1972 A-19
•*Kv?mm!rti!tr*m!**F**!*wi•^v*vKmt !B!BWWiP^W*WWDlIfBfillWWI8Ji
DNA 1948H
P(b, u)
PCA
P.
P'
P
Pa
PN2
Po
pop
pl
Q
Designation on Page 18A-9» of work of Puckett and Teague, from Reference 18A-41 (18A).
Probability for charge transfer on collision at impact parameter "b" and relative velocity "u" (15).
Designation for Polar Cap Absorption (5, 9).
RaU of process "i" leading to electron production (16).
Pressure at altitude (2).
Pressure or partial pressure (3, 8, 10, 20, 21).
Indexing uses: pressure (2). combining proportions (6). projectile species (15). plasma (21). half-integer spacing (21).
Pressure for small perturbation or fluctuation (3).
Mean pressure (3).
Partial pressure for species "a." (3).
Pressure of N^ (20).
Pressure for unperturbed background (3).
Indexing use only; population (4).
Pressure at reference altitude (2).
Diffusional rate (3).
Characteristic Q-number of a resonant cavity (7).
Partition function (11).
Cross-section (15).
Capture cross-section (15).
Source term (21).
Indexing use: quenching (11).
A-20 Revijion No.I, Novtmber 1972
APPENDIX A
Q
Q
Qm^l
Q n
QR
Qrot(X>
Q
Qvib«X)
Q(X)
01 !10
q
Net rate of radiative heat absorption by species "a" (3),
Net rate of chemical energy evolution per unit mass (3).
Source term for electron momentum-transfer collisions {21
Specific slow-ion production cross-section (15).
Net rate of radiant energy absorption per unit mass (3).
Rotational partition function fo..* a rigid rotator (4).
Vibrational partition function (11).
Vibrational partition function for a harmonic oscillator (4).
Partition function of (molecular)species "X" (4),
Ionization cross-section (ambiguous term) where i = j (15).
Cross-section for collisional charge exchange in heavy- particle collisions, where i=n-fj (15).
Cross-section for collisional charge exchange where i= 1 (15).
Total slow positive-"harge production cross-section (15).
Electron production cross-section (15).
Ion-pair production rate due to beta-particle ionization of
Electron production rate (9).
Bremsstrahlung radiation (11).
Electron source function (22).
Indexing use: quenching (9).
Total heat flux vector (3).
Heat fiux carried by species "a" (3).
Revision No.|, November 1972 A-21
»pw^^'5#c^lWJ,«f•'.^^*^?«^B«ww.l^^'w^•'a" iwwijjwfcjswwgpff8^^
s N o-Q. Ä=Or01 at low energies (15).
Vv"
R
Re
Franck-Condon factor for electronic transit., .m involving v=v' in excited state and v=v" in ground state (11).
Gas constant (2, 3, 19).
Designation in Table 9- 5, for resonance scattering process (9).
Interaction distance, in the method of Fleischmann, Dehmel, and Lee (15).
Inter nuclear separation (15).
Indexing uses: radiant energy (3). chemical destruction (11).
Reynolds number (3).
Designation for real portion of function (21).
ReAK- Real portion of AK., in the low-frequency limit (21).
Ri Richardson number (3).
R. l
Ro
Ryd
R. •xM
R Ape
Chemical removal rate constant of species "i" (2).
Impact parameter, in the Firsov model (15).
Indexing use only; Rydberg (11).
Irradiance incident on volume elemer.t \11).
Solar irradiance upon the atmosphere at center wavelength X^ of electronic transition (11).
Radius of interaction (15).
Indexing uses: radiative i «combination (3, 9). recombination (16). reference (16, 19). reverse (ISA).
Position vector measured from earth center (3).
Electron position vector, with respect to trajectory mid- point (1 5).
Indexing use: trajectory midpoint electron position vector (15),
A-22 Rovision No.i, November 19 72
I
APPENDIX A
TID DesigiAäliuii lor iraveling Ionospheric Disturbance (3).
! T. Ion-kinetic temperature (17). ion r x '
!' T. Effective temperatu-e of species "j" (3).
I Tj Fluctuation of T. (3).
T. Mean value of T- (3). j J J
T, Kinetic temperature (4).
\ T, . Kinetic temperature (11).
i j T Molecular-scale temperature (2),
I TM Indexing use only; normalization, in the method of Fleisch-
mann, Dehmel, and Lee (15).
. T Electron noise "temperature'1 (21). i
TOF Designation for Time-of-Flight (7).
1 T Population temperature (4). I pop
I T Reference temperature (16, 19).
| T . Reference temperature (24).
I T Rotational temperature (11). I rot r
1 ~tr .—r^«•~ v~w,.
T Vibrational temperature (4, 20, 24). f v I T Vibrational temperature (11, 18A).
T-V Designation for translational»vibrational energy transfer
i I T, Positive-ion temperature (16).
A-25 Revision No.1, Nrirfombor 1972
iBiiMqgwF^u'^.wiygs^ RBQIpipmMPPIliWPVflll^Q^iP pfSff^pwwwaifsw»«?^?1^
DNA 1948H
th
t o
tot
tr
U e
UHF
UV
u
u
u
u
u
u ~a
u
u. 1
u. 1
Time (2, 3, 5, 11, 15, 16, 19, 20, 21).
Indexing uses: turbulent (2). threshold (6). target species (15),
Indexing use only; thermal (3).
Initial time of integration (21).
Indexing use only; total (4).
Indexing use only; translational (20).
Potential energy of bound electron (15).
Designation for Ultra High Frequency (7).
Designation for Ultraviolet.
Speed (3).
s 2.855 e/X (11).
Relative velocity (15).
Radial component of relative velocity on collision, in the Firsov model (15).
Indexing uses: relative velocity (15). energy exchange (21).
Mean mass velocity (2),
Velocity vector (3).
Veiocity vector for small perturbation or fluctuation (3).
Mean velocity vector (3).
Velocity vector for species !la" (3).
Arbitrary reference velocity (3).
Mean velocity of species "i"' (2).
Directional components of velocity (3),
Mean directional components of velocity (3).
A-26 Revision No.I, November 1972
u O
UV
u
u.
V
V (r ) a* a'
W l
VT
V-T
VV
v
APPENDIX A
Ionizational impact velocity, in the Firsov model (15).
Designation for ultra-violet.
Vertical component of diffusion velocity of atomic oxygen (3).
Vertical component of diffusion velocity of molecular oxygen (3),
Volume (10).
Potential centered on trajectory point (15).
Potential centered on trajectory point (15).
Diffusion velocity of species "i" (2).
Designation for vibrational-transiational energy transfer (20).
Designation for vibrational-transiational energy transfer (11).
Designation for vibrational- vibrat: onal energy transfer (20, 24).
V-V Designation for vibrational-vibrational energy transfer (11).
v Initial velocity (3).
Relative ccliisional velocity (6).
Vibrational level or quantum number (9, 11, 16, 20, 24).
Velocity (15, 21).
Indexing uses: constant volume (3). vibrational (4, 11, 20, 24).
Velocity vector (15).
Velocity vector (15).
Vibrational level in excited electronic state (11).
Vibrational level in unspecified electronic state (20).
Ravivion No.!. November 1972 A -2?
DNA 1948H
e
v1
e
vib
v max
vol
v
v'v" Indexing use only; electronic transition involving two states for which v= vJ and v- v", respectively (11).
v" Vibrational level in gronnd electronic state (11).
Vibrational level in unspecified electronic state (20).
v" Mean number of vibrational quanta excited in ground elec- tronic state through fluorescence (11).
Velocity of bound electron on target atom (15).
Parameter defined in Equation 15-11 (15).
Indexing use only; vibrational (4, 11, 18A).
Maximum vibrational level (11).
Indexing ise only; volume (11).
Velocity of incident ion (15).
vj Parameter defined in Equation 15-11 (15).
W Designation for west (3).
Designation for unspecified chemical species (6, 10).
WB Designation in Figure 16-2, for work of Weiler and Biondi, from Reference 16-24 (16).
W-K Designation for Watson-Koontz system (9).
w Electron drift velocity (21).
X Designation for unspecified chemical species (6, 9, 10, 11, 14, 36, 17, 24).
Indexing --'ses: chemical species (4, 8, 14). functional (21).
fX] Concentration of species "x" (11).
X' Indexing vise only; chemical species for product atom which may be in a bound excited state (8).
A-28 Revision No.1 Novomber 1972
APPENDIX A
(T.. Absorption cross-section for O-, at zero atmosphere pres- sure, by extrapolation (Herzberg continuum) (12).
CT-. A! > (? at low energies (15).
j a„. Electron stripping cross-section from neutrals (15).
J
a Absorption cross-section for O? at one atmosphere pres- sure (Herzberg continuum) (12).
(7, Cross-section for stripping "mrl electrons in N upon N impact (15).
(7 0" in the low-energy limit (15).
T Time for onset of turbulent dispersion (3).
Recovery time (9).
Relaxation time, or the e-fclding time of c (20).
r Effective lifetime for collisionai deexcitation (20).
T.(AA) Optical depth in wavelength range "AA" for species "j" (13),
T Collision-free radiative lifetime of excited species (20). i
T(AA) Optical depth in wavelength range "AA" {13}.
$ Rayleigh dissipation function (3).
$S(AA) Local photon flux in the wavelength range "AA" at altitude "z" (13).
$„(AA) Photon flux in the wavelength range "A A" at the top of the atmosphere (13).
&• Turbulent mixing flux for species "i" (2).
0 Latitude (2, 3).
0-(£ ) Bound-state wavef; nction for the charge state "i" at a trajectory point (15).
(Mrc» r) Wavefunction defined in Equation 15-18 (15).
Revision Not, November (972 A-37
•----•• ^•rsv-1-v<-7»1^'1' *'"'""^''""- --,•,^,;*••"*, -r.n'V-'.''-,-"*-^-'-'',*'r';- IV^1-*-«^ ",--"'-"v-'l.''r •• , •
DNA 1948H
0.(r ) Bound-state wavefunction for the charge .state "j" at a trajectory point (15).
0.(r , r) Wavefunction defined in Equation 15-1° (15).
0 Total wavefunction (.1.5),
Q = co or COico, or CO±co,. (21).
0 Angular velocity of earth's rotation (3).
60 Frequency (3).
Frequency of alternating electric field (7).
Angular frequency of applied electric field (21).
«a - co/2H (3).
CO Cyclotron frequency for electrons in a magnetic field (21),
CO, • Cyclotron frequency for ions in a magnetic field (21).
10c Angular or cyclotron frequency of orbital motion (7).
CO Vibrational constant (4, 11). e \ ' .
CO x First anharmonic correction term (11).
CO Plasma resonance frequency for electrons (21).
CO Wind shear (3). s
Numbers used as indices:
0 Reference condition (3).
Temperature of OK (10, 19).
Zero atmosphere pressure (12).
Initial charge on neutral target species (15).
Zero time (16).
Functional (21).
A-38 Revision No.!, Nov*mb»r 1972
APPENDIX A
Ül Excitation (11).
1 Reference condition (2).
Atomic oxygen (3).
Molecular (3).
Vibrational level (10).
One atmosphere pressure (12).
Incident particles before collision (15),
Cut-off (15).
Stripping, in collision of N on N^ (15).
10 Deexcitation (11).
Deactivation of first vibrational level (20).
2 Molecular oxygen (3).
Turbulent (3).
Vibrational level (10).
Incident particles after collision (15).
Number of electrons stripped, In collision of N on N?
(15).
Two-body process (16).
Functional (21).
3 Vibrational level (10).
Number of electrons stripped, ir. collision of N on N-> (15).
Three-body process (16).
4 Number of electrons stripped, in collision of N on N9
(15).
300 Temperature of 300 K (24).
A-39 Revision No.], November 1972
"»»!>»».» •""—— ~^•.^-.• ^-^^^-^^^,_,:^_ __
DNA 1948H
Misce! symbol
X'
X
X
X
X
(x>
IX]
Top of atmosphere (13).
End of trajectory (15).
Designation of long time after ionizing source is turned on (16).
laneous symbols used as indices (where "X" is taken as an anonymous modified by each index):
Fluctuation or perturbation (3).
Miscellaneous (3)
Reverse (6).
Bound excited state (8).
Collisional (11).
Excited electronic state (1.1).
Ionization (13).
Secondary of a type (14).
Upper electronic state (14).
For special parameter (15).
Unspecified electronic state (20).
Ground electronic state (11).
Lower electronic state (14).
Unspecified electronic state (20).
Vector (3, 15).
Tensor (3).
Vector (15, 16).
Mean (2, 3, 11, 21).
Space-averaged (16, 21).
Variation (3, 16).
A-40 «(»vision No.I, November 1972
APPENDIX F
APPENDIX F
SPECIES INDEX
N. B, : The entries are listed by chapter and page. For instance, the designation 5-7, 8 indicates the presence of informa- tion on pages 7 and 8 of Chapter 5, and 5-(6-9) designates information on pages 6 through 9 of Chapter :5. In a few cases, a species is treated continuously throughout an entire chapter; when this occurs, the chapter number is given. Where information is contained in a figure or table, the figure number or table number is given separ- ately from the chapter and page numbers, which are used only for textual reference. Certain tables are subdivided, e.g., 16-1 into 16- 1. 1, 16-1.2, etc., and 24-1 into Roman Numeral categories. These subdivisions are included in the designations, where applicable, for greater clarity. Entries are listed alphabetically by standard chemical symbol, with the added features that the invented symbol "Me" is used to indicate metallic species generally, and that "air", "air ions", "electron", and "teflon" are entered as words, in their proper alphabetical order. Electronically excited states are listed either as specific state designations (in alphabetical and numerical order) where these are known, or by the use of the asterisk (*) to indicate electronic excitation generally. Vibrationaiiy excited states are designated by the double-dagger ( + ). Unless otherwise noted, all species listed are gas-phase species. A few solids and liquids are included, and are appropriately designated as such, viz. , by the respec- tive standard indicators (s) and (i).
Ag Figure 15-2.
Ag Page 15-36.
F-l Revision No.], Novvmbei 1972
,>• T^-i«yf^v'.-v-.*.-v-FW^^-'-«-' 7' -• .77- ,ri ^m'^'r^^'v WT?,''-','TOtl^»7t'''''; •-^••'•lW\~iwt^-'*-^'y"^J-«W^ig7^. --«hap^vafw«?*"" •T'•*TV7^^^;^*^^^^,**F?w^^
DNA 1948H
Air
Air Ions
Al
Ai
A1(CH 3'3
AlO
AlO
Ar
*
Ar'"
Ar+
Ar + *
Ar 4.+
Ar 3 +
Ar 4+
Ar 5+
Pages 3-5. 33; 5-18; 7-27, 29; 17-7; 21-4, 5, (7-9), (16-18), 25.
Tables 11-2; 16-1.2; 21-2, 4; 24-1 (VI). Figures 7-8; 9-2, 3; 21-3, 5.
Pages 16-21, 23. Tables 16-1. 1; 24-1 (VI).
Pages 5-13; 7-20; 15-1, 21, 29. Figures 5-10; 15-1, 5.
Pages 15-6, 15, 31, 35, 39, 44, 45, 47; 16-18; 20-18. Table 16-1.1. Figure 15-4.
Page 5-19.
Pages 11-23, 25. Table 11-1.
Page 11-2 5.
Pages 2~(9-12); 4-1; 10-2; 11-27; 15-21, 25,
34, 36, 37, 43; 16-14, 16, 17, 24; 17-3: 18A-9; 19-8, 9, 12; 21-5, 24.
Tables 2-2, 4; 10-1, 10; 15-1; 18A-5; 20-2, 6, 8; 24-1 (XXVI).
Figures 2-7; 4-1; 10-10; 14-10; 15-1, 2, 5.
Table 10-10.
Pages 15-31. 43: 16-1H. Tables 10-1, 11: 16-1.1.
Table 10-11.
Page 15-43. Table 10-1.
Page 15-43.
Page 15-43.
Page 15-4 3.
F-2 R-.3vit.on No.I. November 197?
p'>,.--y ,.•-JTC •<*->>*,, i.-lF-^."
APPENDIX F
Cs Pages 15-37, 41. Table 20-10.
D Pages 16-22, 23, Table 16-1.2.
D Page 16-24.
Electron Chapters 17; 21. Pages 4-6, !3; 5*45-8}, 19; 6-2, 3. (7-12), 14; 7-2, 4,
8, li, 20, 23, 25, 27, 29; 8-{l-7), 10, lij 9-1. 4, 6, (8-16), 30; ll-(25-33); 12-1, 5: 13-1; 15-1, (5-7), 20, 25, (29-47); 16-(1-21); 20-3, 5, 7, 8, 10, 11, (13-17); 22-2.
Tables 6-1; 8-(l-3); 9-1. 4; 12-1; 16-1. 1; 18A-4; 20-7, 9, 10; 24-1 (I, II, III, IV, VII, VIII, IX, X, XI, XII, XXX).
Figures 4-3; 5-9; 7-6, 7; 9-1; 14-17; lo-(l-4); 20-(3-5):
(7-9).
F
Page 17-18. Table 17-7. Figures 15-1, 2.
Page 16-18. Table 16-1.1.
Fe Pa^es 11-20; 15-1, 21, 30; 20-7. Tajle 18A-7. Figures 15-1, 5.
Fe Pa^es 15-6, 15, 32, 3b, 40, 44, 4b, 47; 20-iö. Tables 3 8A-3, 5, 7; 24-1 (XIV). Figures 15-3; 20-1.
FeO Page 11-20. Table 11-1.
FeO Tables 18A-3; 24-J (XIV),
FeO. Table 18A-5.
Revision No.!, November 1972
F-7
DNA 1948H
H
H"
2 H{ 3 P)
H(2S)
Pages 2-9, 12; 6-8; 7-7; 8-(6-8); 10-4; 1 i-1 5, 17; 15-1, 18, 19; 19-3, 12; 20-16.
Tables 6-1; 8-2; 9-1, 5, 6; 10-1, 2; 12-2: 18A-(l-4), 7; 19-1; 20-10; 24-1 (I, IV, XIII, XIV, XV, XXIV, XXV, XXVII).
Figures 2-7; 10-1, 10; 14-1, 3, 4, 17; 15-1, 2.
Tables 10-2; 20-10. Figure 10-1.
Tables 9-5; 20-10.
Table 20-10.
H
H
HCO
HNO
HNO
•f
3
Pages 6-8; 7-17; 8-1, 8, 9-6, 8; 10-3; 16-18, 20, 22, 23.
Tables 8-1; 9-1; 10-1; 16-1.1, 1.2; 18A-1, 3, 7; 20-10; 24-1 (I, XIII).
Figures 14-3, 4, 64, 89; 16-4.
Pages 7-17; 8-6, 7; 10-3; 16-22, 23; 17-2, 8. Tables 10-1; 16-1.2; 17-3; 18A-2; 24-1 (XV). Figures 10-9; 14-1, 16.
Sec CHO+
Page 18A-9. Tables 18A-3, 4; 24-1 (XIV).
Page 11-13. Table 11-1.
HO. <
HO' t
HS
HS"
Pages 2-9; 11-16; 19-12; 20-16. Tables 11-1; 19-1; 21-1 (XII, XXIV, XXV, XXVII)
Page 17-2.
Table 18A-2.
Table 18A-2.
F-8 fltvijior« No.I. November 1972
APPENDIX F
H. Pages 2-9; 10-2; 11-31, 33; 16-17, 18, 24; 17-4; 19-4, 12; 20-16.
Tables 9-5; 10-1, 19; 17-4; 18A-3; 20-10; 24-1 (XII, XIV, XXV, XXVII).
Figures 10-8; 14-(12-20); 15-1, 2.
H. Table 20-10.
H,
H. + *
Page 16-18. Tables 10-1, 19; 16-1.2. Figures 14-13, 64, 89.
Page 16-18.
H,
H2N°2
Page 17-9.
See NO+(H O).
H2N03 See NO (HO). Ct C*
H2N04
"2°
See NO (H„0).
Pages 2-9; 4-15; 6-8; 9-11; U-1, 11; 12-6, 29; 17-3, 4, 8, 12; 18A-2, 3, (8-10); 19-12; 20-15, 16; 21-5, 6, 8, 16, 18, 27, 28.
Tables 6-1; 10-1, 20; U-1, 2; 12-2; 17-(3-5), 7; 18A-1, (3-7); 20-5, 6, 8, 10; 21-1, 2; 24-1 (IV, IX, XII, XIII, XIV, XVI, XVIII, XIX, XXI, XXIV, XXV, XXVII, XXX, XXXIII).
Figures 4-2, 8; 11-1; 12-17; 14-(62-65); 20-6; 21-1, 3, 5.
H20 Page 4-15. Tables 10-20; 20-5; 24-1 (XXXIII).
H2°
H.O + *
Tables 10-1, 20; 18A-1, 3, 7; 24-1 (XIII, XIV), Figure 14-63.
'1'able i0-20.
H20 Page 17-9.
H2°2 Page 2-9. Table 24-1 (XXIV, XXVII]
Revision No I. Nov«mber 1972 F-9
DNA 1948H
H2°2 See °~<H2°>-
H2°3 See °2(H20)'
H£0~ See o'(H O).
H2°4 See 03<H20)-
H2SO (X) Page 19-4.
H30 Table 18 A-7.
H30 Pages 9-11; 16-17; 18A-8; 21-20. Tables 16-1.1; 18A-3, 5, 7; 21-4; 24-1 (IV, XIV,
XVIII, XIX).
H30" (HO) Pages 18A-8; 21-25. Tables 16-1.1; 18A-3, 5; 21-4; 24-1 (IV, XIV, XVIII,
XIX).
H30+(H20) Pages 16-17; 18A-9.
Tables 16-1.1; 18A-3, 5; 24-1 (IV, XIV, XVIII, XIX).
H30+(H20)3 Tables 16-1.1; 18A-5; 24-1 (IV, XVIII, XIX).
H30+(Ha0)4 Tablrs 16-1.1; 18A-5; 24-1 (IV, XVIII, XIX).
H30+(H O)^ Page 16-17.
~ Tables 16-1.1; 24-1 (IV).
H 0+(H O) Pages 9-11; 16-17; 18A-8; 21-20. n Tables 16-1.1; 24-1 (IV, XVIII, XIX).
H30 (OH) Page 18A-8. Tables 18A-3; 24-1 (IV, XIV, XIX).
H^O" See OH~(H20).
H3PO (X) Page 19-4.
H.Not See NO+(II,0)_. 4 3 2 '2
H40* See H^/'OH).
F-10 Revision No.l, Mov«mb«r 1972
APPENDIX F
4 4
H6N°4
H8°;
H10°7
Hll°5
H13°6
H, NO" ,
H-, O" , 2n n+2
H2n+3°+n+l
He
See 0-(H20)2.
See H 0+(H20).
See NO+(H O) .
See 0-(H20)3.
See H30+(H20)2.
See 0-(H20)4.
See H30+(H20)3.
See 0"(H„0) . C. L. o
See H30+(H20)4.
See H30+(H20)5.
See NOJHO) .
See Ol(H-O) . 2 2 n
See H,0+(H.*Ö' . 3 2 n
Pages 2-(9-12>; 4-1; 7-4, 10, 23; 8-4; 11-33; 15-1; 16-12, 14, 15, 17, 20, 21, 24; 18A-4, 7, 9; 19-12; 20-15; 21-17.
Tables 2-2, 4; 8-2; 9-1, 3, 5; 12-2; 16-1. 1, 1.2;18A-1, 5, 6; 20-8, 10; 21-3; 24-1 (XVIII. XXI),
Figures 2-7; 4-1; 7-3, 6; 15-1, 2; 21-4.
• e
He( P*
He(2 lS)
He(3S)
Table 20-10.
Table 9-5.
Table 20-10.
Tables 9-5; 20-10.
He Pages 8-3; 15-45, 46; 16-18, 20, 22, 23; 18A-3, 4. Tables 9-1, 3, 5; 16-1. I; 18A-1; 20-10.
R«viiion Mo.I. Novernbar 1972 F-ll
DNA 1948H
He, Page 16-20. Tables 16-1. I; 18A-1,
Hg Page 20-7.
I Pages 15-21; 19-3. Table 18 A-2. Figures 15-5, 7.
_+ Pages 15-37, 41. Table 15-1.
Page 16-21. Tables 16-1.2; 18A-2,
Page 16-21.
Page 16-21. Table 16-1.2.
K Pages 15-21, 29. Table 8-2. Figures 15-2, 5, 8.
K Table 9-5.
K Pages 15-32, 35, 40; 16-18. Tables 15-1; j6~l. 1; lgA-3,5,
K"\'CO2) Table 18A-5.
KO+ Table 18A-3.
Kr Pages In-30; Table 20-8.
16-24.
Figures 15-1 •?
Kr + Pages 15-32, 36, 4C
JLi Page 15-1. Table 8-2. Figures 15-1, 2.
Li Table 9-5.
F-12 Rev.s.on No.], November 1972
••».v»Ti ••••"-:•?''
APPENDIX F
N, Pages 2.(9-12); 4-1, 8, 13; 6-8, 14, 15; 8-11, 12; 9-4, 12, 13, 31; 10-2, 4; 11-13, 14, 18, 27, 32; 12-6, 16, 17, 30; 13-(l-4); 14-1; 15-1, 21, 22, 25, (34-38); 16-8, 10, 22, 24; 17-3, 5, 8; 18A-(3-5), 7, 9; 19-4, (7-10), (12-14); 20-(3-10), 13, (15-17); 21-4, 5, 8, 15, 20, 25, 26, 28, 31; 22-1.
Tables 2-2, 4; 9-2, 3, 6, 7; 10-1, 13; 11-2; 12-(2-4), 6a, 6b; 13-1, 2, 4, 6; 14-(l-3); 15-J; 16-1.2; 17-(4-6); 18A-1, (3-7); 19-1; 20-1, 2, (4-6), (8-10); 23 -(1-4); 24-1 (I, II, IV, IX, X, XII, XIII, XIV, XVI, XVIII, XXI, XXIII, XXIV, XXV, XXVI, XXVII, XXVIII, XXX, XXXII, XXXIII).
Figures 2-7; 4-1, 4, 8; 10-5, 8, 11; 12-7; 14-(29-4I); 15-1, 2, (6-9); 20-1, 3, 4, 6; 21-1, 3, 4.
N, Pages 4-13; 5-17; 6-7; 11-14, 34; 19-7, 14; 20-(3-6); 21-4; 22-1.
Tables 9-6; 20-2, 3, 10; 24-1 (XXVII, XXXII, XXXIII).
Figures 10-5; 20-1, 3, 4.
N. Pages 20-3, (6-8). Tables 10-13; 20-I, 10. Figures 10-5; 20-1.
N.(a n ) 2 g
N2(.AV)
3 + * N2(A £ )
Tables 9-5, 6; 10-13; 20-1, 10. Figure 10-5.
T»-, Ulo Tfl i r\
Tables 10-13; 20-1. Figure 10-5.
Pages 6-15; 20-3, (6-8). Tables 9-6, 7; 10-13; 20-1, 4, 10; 24-1 (XXVIII, XXX). Figures 10-5; 20-1.
Pages 20-3, 7. Figure 20- 1.
H (b' Lu) Figure i0-5.
Revision No.I. November 1972 F-19
DNA 1948H
N2(B n ,
N2(B" V>
N2(C nu)
N2(C 3n/
N2(C \)
N2(D V)
N2(E V)
Vh ^ u' 1
N2(w Au)
N2(W Au)
Pages 6-15; 20-6, 7. Tables 9-5, 6; 10-13; 20-1, 10; 24-1 (XXV). Figures 10-5; 20-1.
Figure 20-1.
Page 20-7. Tables 9-5; 10-13; 20-1. Figure 10-5.
Pages 20-6, 7. Tables 9-5, 6; 20-10. Figure 10-5.
Table 20-10.
Figure 10-5.
Page 20-7.
Page 20-7. Figure 10-5.
Tables 9-6; 12-6a.
Tables 10-13; 20-1. Figure 10-5.
Page 20-7. Tables 10-13; 20-1.
N2< "u1
+ N2
Tables 12-6a, 6b.
Figure 10-5.
Pages 6-15; 8-12; 9-4, 11, 21, 31; 13-1, 3, 4; 14-1; 15-5, 43; 16-7, 8, 10, 18, 22; 18A-(4-7); 20-(6-J0), li>, 17; 21-20.
Tables 9-2, 3, 6; 10-1, 14; 13-3, 5, 7; 14- i, 2; 16-1.1, 1 2; 18A-1, 3, 5, 7; 20-1, 9, 10; 21-4; 24-i (I, II, IV, V, XIII, XIV, XVIII, XXX).
Figures 10-5; 12-7; 14-(30-37,, 90; 16-1; 20-2.
-20 Revision ,-o.l Nover-be/ 197/
APPENDIX F
N3
Na
Na
Nd
Na (CO )
Na+(CG2)2
NaO
Me
Ne""
Ne
Ne ++
Ne3+
NT 4+ Ne
Ne 5+
Ne.,
Pages 16-7, 8, 10; 20-9. Tables 18A-3; 2i-4; 24-1 (IV, XIV, XVIII).
Pages 16-7, 10, 16; 18A-7. Tables 16-1.1; 18A-1, 3, 5; 21-4; 24-1 (IV, XIV,
XVIII). Figure 16-1
Pages 5-19; 18A-3, 6; 20-7. Tables 8-2; 9-6; 18A-1, 3, 7; 20-10; 24-1 (XIII, XIV), Figures 15-2; 20-1.
Tables 9-5; 20-1, 10.
Pages 16-18, 23; 18A-6; 20-18. rabies 16-1.1; 18A-1, 3, 5, 7; 24-1 (XIII). Figure 20-1.
Table 18A-5.
Table 18 A- 5.
Tables 18A-3; 24-1 (XIV).
Pages 15-25, 43, 44; 16-8, 10, 11, 14, 16, 24. Tables 8-2; 15-1. Figures 15-1, 2.
Page 16-8.
Pages 15-34, 39, 43; 16-18. TaTjl« 16-1. 1.
Page 15-43.
Page 15-43.
Page 15-43.
Page 15-43.
Page 16-16.
Revision No.l. November 1 772 F-23
DNA 1948H
O Pages 2-(9-12); 3-33, 34; 4-13, 15; 5-18; 6-2, 8, 12, 14, 15; 7-7; 8-7, 8, 10, 11; 9-12, 13, 15, 30, 31; 10-4; 11-13, (16-20), 31, 32; 12-6, (8-23), 30; 13-1, 3, 4; 15-1, 6, 15, 25, (29-33); 16-10, 11, 16; 17-2, 6, 9, 12, 14; 18A-5, 6, 8; 19-(2-14); 20-3, 6, 7, (10-12), (14-18); 21-6, 16, 20, 25, 29.
Tables 2-2, 4; 6-1; 8-2; 9-(2-6); 10-1, 8; 12-(l-5), 7a, 7b, 8a, 8b; 13-1, 2, 4, 6; 15-2; 17-(l-4), 6, 7; 18A-(l-4), 6, 7; 19-1; 20-1, 2, (4-7), 9, 10; 21-(l-4); 24-1 (I, II, IV, V, VII, VIII, IX, X, XI, XII, XIII, XIV, XV, XVI, XVIII, XXIII, XXIV, XXV, XXVI, XXVII, XXVIII, XXX, XXXII).
Figures 2-7; 4-1, 7; 10-3, 6, 7, 10; 12-(8-10); 14-2, (7-9); 15-(l-4); 20-1, 4, 6, 9; 21-1, 4.
o"~
0(2D)
0(4 P)
Pages 12-(17-23). Tables 10-8; 12-5; 20-1, 7, 10. Figures 10-3; 12-8, 9; 20-1, 9.
Pages 4-13; 5-17, 18; 6-15; 8-10; 12-9, 21, 27, 28; 16-16; 19-14; 20-3, 4, 12, (14-16); 22-1.
Tables 9-(5-7); 12-3, 5, 7a, 7b; 20-1, 7, 8, 10; 24-1 (IV, XXIV, XXVII, XXVIII, XXX).
Figures 4-2, 4, 5; 10-6, 7, 10; 20-1, 9.
Table 9-5.
0(DP) Table 9-6.
o.' st Pagco 5-IG, 0-10, 9-3i; IZ-Zl; ib-ib; 19-14; 2^-4, 14, 15. Tables 9-(5-7); 12-7a, 7b; 20-1, 7, 10; 24-1 (IV. XXV,
XXVIII, XXX). Figures 10-6, 7; 12-10; 20-1, 9.
0( S^
0( °S)
Tables 9-5, 6; 20-1.
Tables 9-5, 6; 20-i. Fig u r e 20-1.
O Pages 4-6; 6-7, 14, 13; 8-2, 8; 9-(ll-13), 15; 10-4; 12-14, 21; 13-3, 4; 15-31, 34, 59, (43-45), 47; 16-18, 22, 23; 18A-5;20-5, 11, (15-17).
F-24 Revision No I. November 1972
APPENDIX F
CT (Cont'd.) Tables 9-2, 3, 5, 6; 10-1, 9; 12-1, 7b, 8a, 8b; 13-3, 5, 7; 16-1.1, 1.2; 18A-1, 3, 5, 7; 20- 5 3; 21-4; 24-' (I, II, V, XIII, XIV, XVIII, XXVIII, XXX).
Figures 4-3, 4; 10-4, 6, 7; 12-8, 10, 11; 14-8, 64, 73, 74; 20-2, 4.
+ * O
OVD)
OVP>
+ 4 O ( P)
o ++
Pages 12-20, 21; 20-(15-l7). Tables 10-9; 20-1. Figures 10-4; 12-(8-l.l); 20-2,.
Pages 6-15; 12-20; 20-8, (16-18). Tables 9-3, 6; 12-8a, 8b; 20-1, 9, 10; 24-1 (II, XIII,
XXVIII, XXX). Figures 10-7; 12-8, 9, 11; 14-73; 20-2.
Pages 12-21; 20-16, 17. Tables 9-6; 12-8a, 8b; 20-1; 24-1 (II, XXVIII). Figures 12-(9-ll).
Figure 14-74.
Page 15-43. Tables 10-1; 12-1.
O
o"
Page 15-43.
Pages 5-7; 6-12, 14; 8-7; 9-15, 30: 10-3; 11-25; 16-22, 23; 17-2, 4, 5, 8, 9, 12, 13; ISA-3; 20-11, 13.
TaM.-i 10.1. 7; TA-!.2; 17(1 1), 6, 7; 18A-2, 4, 6, 20-10; 2-4-1 (V, VII. VIII, IX, X, XI, XII, XV XVI, XX, XXI).
Figures 10-6, 7, 9; 14-2.
o Table 10-7.
o'(co2) >ee CO~
o~mo) Tables 18A-6; ; 24-1 (XXI).
ocs Page 19-6.
Revision No.l, Novombor 1972 F-25
DNA 1948H
OH Pages 2-9; 7-7; 11-1, 16, 17; 17-2; 18A-8; 19-3, 12; 20-16; 21-6.
Tables 6-1; 10-1, 19; 11-1; 17-{l-3); l8A-(l-3); 19-1; 20-10; 24-1 (VII, WH, Xlll, XiV, XV, XIX) XXIV, XXV, XXVII).
Figure 4-6.
OH Pages 11-{15-17). Tables 9-5; 20-10.
OH' Page 12-29. Tables 10-19; 20-10.
OH
H OH
OH"
.+*
Tables 10-1, 19; 18A-1, 3; 24-1 (XIII, XIV). Figure 14-64.
Table 10-19.
Page 17-2. Tables 10-1, 19; 17-1, 2, 7; 18A-2, 4; 24-1 (VII, VIII,
XII, XV).
OH (H20)
OONO" (Cf.NO~)
O.
Table 17-7.
Page 18A-7. Tables 18A-4; 24-1 (XVI).
Pages 2-(9-H); 3-33, 38; 4-1, 6, 8, 10, 15; 5-19; 6-2, 8, 12, 14, 15; 8-11; 9-12, 15, 30; 10-2, 4; ll-(13-20), 27, 32, 33; 12-(6-16), 20, 27, 28, 30; 13-1, 3, 4; 15-1, 21, 34, 36, (39-43), A f .4-1 y / \ A i r i -» -> ~» i"> i-io A i / r\\ TU, "* ' , IU"i"I| A ~> • A«, C L. , <-••'> A I "* i., TC, \U ~ O / ,
12, 14, 17; 18A-(5-9); 19-(4-6), (8-14); 20-6, (9-18); 21-4, 5, 8, 16, 20, 25, 27, 28.
Tables 2-2, 4; 9-2, 4, 6, 7; 10-1, 17; 11-2; 12-(l-4), 7a, 7b; 13-1, 2, 4, 6; 15-1; 16-1.2; 17-(l-7); 18A-(l-7); 19-1; 20-1, 2, (4-6), (8-10); 21-( 1-4); 24-1 (I, II, IV, VII, VIII. IX, X, XI, XII, Xllt, XIV, XV, XVI, XVIII, XIX, XX, XXI, XXII, XXIII, XXIV, XXV, XXVI, XXVII, XXVIII, XXIX, XXX, XXXII, XXXIII).
Figures 2-7; 3-7; 4-1, 4, (6-8); 10-7, 8, 11; ll-(8-10) 12-(l-6); 14-(45-61); 15-1, 2, (6-8); 20-1, 4 (6-8); 21-1, 3, 4.
F-26 Revision Not, November 1972
APPENDIX F
°2<H20)
°2(N2)
<X(No0)
°2<02>
o. ++
Page 18A-8. Tables 18A-3, 5; 24-1 (IV, XIV, XVIII).
Tables 18A-3, 5; 24-1 (XIV, XVIII).
Table 18A-5,
See O.. 4
Table 10-1.
O, Pages 5-7; 6-12; 9-30; 16-22; 17-2, 4, (7-9), (12-14); 18A-3, 7; 20-13.
Tables 9-4; 10-1, 19; 12-1; 16-1.2; 17-1, 2, (4-7); 18A-2, 4, 6; 20-10; 21-4; 24-1 (V, VII, VIII, IX, X, XI, XII, XV, XVI, XXI, XXII).
Figures 10-7, 9.
°2<CCV 0-(H20)
See CO . A.
Pages 17-2, 9, 17. Tables 17-7; 18A-4, 6; 24-1 (XVI, XXI).
°2(H2°>2
0-(H20)3
°2(H20,4
0-(H?0)5
°2(h20>n
°2(N2>
°2<°2>
o.
Tables 17-7; 18A-6; 24-1 (XXI).
Table 17-7.
Table 17-7.
Table 17-7.
Page 17-16.
Tables 18A-6; 24-1 (XXI).
See O", 4
Pages 2-9-12); 4-15; 5-18; 6-2, 12; 9-30; 11-1, 11, 15, 17, 19; 12-6, 24, 27; 17-2, 4, 9, 12; 18A-6. 8; 19-2, (4-8), 14; 20*12, 13; 21-17.
Tables 2-2: 10-1, 20; 11-1; 12-2; 1 7-(1 -4), 7; 18A-(2-4); 19-1; 20-6. 10; 21-2; 24-1 (VII, VIII, XI, XII, XIV, XV, XVI, XXIV, XXV. XXVI, XXVII, XXX),
Figures 2-7; 4-2, 7, 8; !l-i, 2; 12-14, 1 ^; 21-3.
H«vj$ion Not, November 1972 F-29
DNA 1948H
O.
o+
3
O + *
Page 11-19. Table 10-20.
Page 16-14. Tables 10-1, 20; 24-1 (XVIII).
Table 10-20.
O.
o. -*
Pages 17-2, 9, 12. Tables 10-1, 20; 17-1, 2, 4, 7; 18A-2, 4, 6; 21-4;
24-1 (VII, VIII, XII, XV, XVI, XX, XXI).
Table 10-20.
03(H20)
o'; 4
°4
+ P
PH'
Pt
Rb+
s4
SFÜ
Tables ISA-6; 24-1 (XXI).
Page 20-13.
Pages 16-14, 16; 18A-(6-8). Tables 16-1.1; 18A-3, 5; 21-4: *4-I (IV, XIV, XVIIi,
XIX).
Pages 17-9, 14, 17; 18A-7. Tables 17-7; 18A-4, 6; 21-4; 24-1 (XVI, XXI, XXII).
Page 16-18, Table 16-1.i.
Page 7-9.
Page 7-22.
Page 15-36.
Page 16-18. Table 16-1. 1.
Page 17-18. Table 17-7.
SF, b
Pages 17-j 7, 18, Table 17-7.
F-30 Revision Mo.1, NovBfnfc«, ]972
APPENDIX G
Aubrey, B. B. : 21-7
Awajobi, O. A. : 9-34
Axworthy, A, E. , Jr.: 19-4
Bachynski, M. P. : 2:-10
Badger, R. M. : 20-32
Bahr, J. L. : 12-88
Baiamonte, V. : 6-17
9-19, 27; 17-10; 20-203; 21-61
9-22
17-25
21-16
Bailey, A. D. :
Bailey, D. K. :
Bailey, T. L. :
Bailey, V. A. :
Bair, E. : ^-17
Baisley, V. C. : 12-72
Laker, A. D. : 7-78
Baker, C.: 7-78
Baker, D.M.: 3-33; 20-166
Baker, K. : 20-166
Baldeschwieler, J. D. : 7-22
Baldwin, R, R. : 19-33
Bamiord, C. H. : 11 - 18 { Ed. )
Banks, P. : 21-70
Bardsley, J. N. : 8-13, Zl, 61, 64; 11-66; 16-28; 17-39, 60
Barrow, R. F. : 10-32
Barth, CA.: 9-74, 92; 19-35; 20-69
Basco, N. : 20-217
Bates, D. R. : 4-4 (Ed. ); 7-9 (P:d. ), 57 (Ed. ), 89 (Ed. ); 8-1, 4, 6, 7, 8, 9, 10, 12, 14, 16, 17, 25, 26, 30; 9-25: 11-68, 69; 15-2 (Ed.), 4, 19, 20 (Ed. ), 32; 16-42 (Ed. ), 43; 17-21; 20-4, 43, 76, 235
Bauer, E. : 3 (Author) -2, 44; 4 (Author) -14, 15; 20-6, 7, 55, 56, 80, 143, 222, 2 32
R«vi:;ion No.I, November lb72 G-3
DNA 1948H
Bauich, D. L. : 15-54; 24-16, 35, 32
Baum, C. E. : 21-58
Baurer. T. : 1 (Author); 6 (Author); 19-37; 23 (Author); 24 (Author
Bayes, K. : 20-155
Beaty, E.G.: 10-36; 17-5, 44, 45; 21-41; 24-3
Beauchamp, J. L. : 7-20, 21; 21-74
Becker, R. A. : 7-70; 12-42
Bederson, B. : 7-2 (Ed, ), 58 (Ed.); 21-7
Bekefi, G. : 21-45
Bell, G. : 15-13
Belles, F. E. : 20-236
Belon, A. E. • 9-11
Belrose, J. S. : 5-14; 9-95; 21-29
Belyaev, V. A. : 7-61
Benesch, W. : 10-52; 20-19
Bennett, R. A. : 17-40, 62
Bennett, W. R. : 20-46 (Ed.)
Benson, S, W, : 19-4
Berkowitz, J. : 7-85; 17-58
Berlande, J. : 16-47
Berning, W. W. • 9-53
Bernstein, R. : 20-220
Berry, R. E. : 16-40
Berry, R. S. : 7-64; 8-75; 10-14, 43; 16-62
Bethe, H. A. : 11-44
Bethke, G. W. : 12-15
Beyer, R. A. : 18-65, 66
Eeynon, W. J. G. : 9-58 (Ed.), 62 (Ed.)
G-4 n«vision No.I, November (972
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