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8/20/2019 Kotelnikov Radio Commn
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RADIO COMMUNICATION
WITH EXTRATERRESTRIAL CIVLIZATIONS
V.
A. KOTEL NIKO V
Ins t i tute of Radio Engineering and Electronics
USSR Academy of Sciences
The aim of this pap er is to con sider the possibi litie s of comm unication
with extra terres tr ia l civilizations whose technology is an outgrowth of
scientific pr inciples that a re already established on the Ear th and which
lead the Ea rth civilization by a few decades.
The Ea rth technology
is
assumed on the present-day level.
Although som e civilization s a r e probably
m or e advanced than we ar e by thousands o r even millions of ye ar s, our
res tr ic ted approach is apparently not unreasonable.
This paper does not
pretend to completeness: it only discus ses some par ticu lar exam ples,
which ar e not meant a s illustrations of optimal case s.
Let us consid er the tra ns mi ssi on of s igna ls in the fo rm of long mono-
chrom atic train s of pulses.
This technique
is
no le s s noiseproof than
othe r methods of transm issio n, and yet it i s s imp ler to achieve; ther efor e
it will probably be adopted in the beginning by young civilizations for
purposes of in ter ste lla r communication. The signal frequency
is
of course
not known in advance, and it m ay change when information i s being tr an s-
mitted.
In this ca se, the optimal recei ver w ill have a circu itry like that
block-diagrammed in the figure.
Her e A is the amplif ier, which may include a frequency changer; fi lt er s
with a band
f
overlapping the ent ire frequency range; D detectors; I inte-
gr ato rs which reco ver the energy passing through the filt er during the
integration time
T
NE suitable nonlinear elemen ts whose outputs a r e
added. A sign al
is
registered when the output of this receiver exceeds a
cert ain value.
F o r simpli city , without sacrif icing much of the noiseproof p rop ert ies
of the r ec ei ve r, the nonlinear elem ents can be repla ced with threshold
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device s which produce an output signal only if the os cilla tory e nerg y
passing through the f i l te r in the t ime
T
ha s exceeded a cer tain threshold
value. I t i s this par t icula r receiver scheme that is conside red in what
follows.
Let the transmitting and the receiving antennas with effective surfaces
S and
S
be pointed at one anothe r. The maximum re ception range
is
then given by
where
P
i s the t r ansm i t t e r power,
the w avelength,
k =
1.38
~ / d e ~ ,
T rec eiv er noise temp erature; i s a function of
Af
the number of filters n
and thresho ld settin g, which depends on the probability of false response p f r
and the permissib le probabil i ty of s ignal loss by the rec eiv er ,
psi
When
con side red a s a function of hf Y ha s a minimum for
17.
F o r
p r
and
psl
le ss than lo-' , i t i s given by
sl
In some case s ,
when
T
i s l a rge , A f cannot be made e qua l to
I/?
s ince
due to the intr insic frequency drif t the signal will m is s the narrow p ass-
band of the fi lt e r. With A f > l / r we have
It i s undesirable to have f
< I / r
since th is wil l com plicate the design
and increa se Y , i . e. , reduc e
R.
We now consider a particular example.
Let the t ra nsm it ter power
commanded by an ex t ra ter re s t r ial c ivi l izat ion be
P=
l o 9 watt (1 of the
ele ctr ic power req uire me nts of the
USA .
The effective surface of the
transmitt ing antenna is
and the effective surface of our receiving antenna is
Set noise
T 30 .
Receiving antenna s with the se pa ra m et er s can be built without much
difficulty.
Tra nsm issio n wavelength
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Fo r a frequency d rift of lo- (which
is
readily attainable at present),
we obtain for the filt er passband
With this passband we may tak e T ~ f
utting 7 1800 sec, pf = p S
and
l o 9 ,
we find
Fro m relat ion A) we then have
o r 128,000 light ye ar s, which is m or e than the di am ete r of the Galaxy.
If information is sent through this line, and the signal frequency is
changed fro m tran smi ssio n to transmission, the information rat e
is
I%?
1/60 bi ts per sec.
r
1800
The information ra te rapidly in cr ea se s a s dec reas es. If we put
T = A f - I = 3 3 sec, and pf =psl =
n 10 a s befo re, we find Y 3
and
R
1oZ0m,o r 10,000 light yea rs.
The corresponding information
ra t e i s
an
@ 9 bifs per set
T 3 3
F o r distan ces of 100 light year s,
T
can be reduced by four or de rs of
magnitude, and the information rat e will approximately increa se to the
sa m e extent.
The receiver being considered is provided with fairly narrow-band
f i l t e r s .
The transmitter and the receiver both accelerate and decelerate
due to the motion of the home plan ets in spa ce , and thi s obviously changes
the frequ ency of the signal.
These frequency changes must be compensated
on location, since otherwise the signal may mi ss the fi l te r s narro w pass-
band.
The compensation can be read ily introduced sin ce the accel erati on
of planetary motion is known at each point.
The ver y larg e number of sep arat e channels in the rec eiv er ( se e figure)
can be apparently replaced with a sim pler device performing the s am e
function.
How a re we going to find a s ta r with a powerful tran sm itt er located
on one of its planets?
Suppose that the tran smitting civilization has built a tra ns mi tte r with
the param ete rs from the previous example,
i e . , P
l o 9
W, S = lo5m2,
0.1 m. The antenna
is
pointed alternatively at different st a rs o r is
allowed to sc an the entire ce lestial sphere, drift ing acr os s a single st ar
In, say,
T
3 sec . Fo r l a rge
7
the problem is even simp ler.
X
The antenna beam fills a solid angle -- and it therefore
scans the en t i re
SI
celestial sph ere in the t ime
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Fo r the above numerical p ara me ter s, we find 2 = 3.8 -10' s e c o r
2
years .
A considerably sho rter t ime is obtained if the antenna is pointed at
a certain s ta r and then rapidly switched to another sta r, etc.
The scanning
tim e fo r all the 10' s t a r s within the radius of 1000 light ye ar s is
T
3.107sec , o r 1 year .
If we assu me that a pre lim ina ry selection of the most promising
s t a r s reduces the population to 1 of the total ten millions, the scanning
time drops to T = 3 l o 5 se c, o r some four days. The scanning time
dec rea ses proportionately fo r st el la r populations within sph ere s of sm alle r
radii .
The technique of rapid antenna switching fr om one s t a r to another
thus redu ces the scanning tim e to a reasonable level.
Let the receiving sy stem be an ar ra y of beamed antennas cov ering the
entire celestia l spher e. In this case, a tran sm itte r with the above par a-
m et er s can be detected at a distance of 1000 light yea rs if the receiving
antenna sur fa ce , accordin g to equation (A),
is
S = 100m2,
It is assumed
that the re ceiver functions a s indicated
in
the figu re and that f T - I ,
T = 30'.
Seeing that the be am of thi s antenna occup ies a so lid angle h z / S
we find that
ar e required to cover the entire celestia l sphe re.
In this arrangement, the antenna is not expected to trac k the st ar . Each
antenna may therefor e have a s many as ten beam s. The number of
individual antennas may th ere for e be substantially le s s than m .
The
numb er of receivin g channels, howe ver, mu st be exactly
m
and each
receivin g channel should be equipped with fi lt er s overlapping the ent ire
relevant frequency band.
If we assu me that the transm ittin g civilization is sufficiently advanced
and its astron ome rs can actually sele ct the
1
of s t a r s which in principle
may support Earth-type civilizations, the scanning of al l the selected
s t a r s within a sph ere of 1000 light ye ar s r adius will take about four days.
The en tire c ele stia l sph ere need not be scanned at one time: different
a re a s of the sky, say , those having differen t declinations, can be scanne d
at different t imes .
Thus, if the sky is divided into 10 ar ea s, the su rv ey of
each ar e a can be completed in, sa y, one month (the signal, if any, w ill be
detected times during this period), and the entire celestia l sphe re will
be scanned in approx imately one ye ar . The num ber of receiving channels
and antennas can be further reduced by one order of magnitude.
The above receivin g network, though by no mea ns cheap o r eas y to
build, can be erected on Ea rth ,
This system wil l detect ext raterre str ia l
civilizations which have transmitters with the above parameters and are
located within the radius of 1000 light ye ar s from the Earth. Since th er e
ar e near ly
lo
s ta r s within this sp here, the sea rch will be success ful if
at lea st one of the ten million st ar s has a t ran sm itte r of the required kind.
If the distance scale i s reduced, the sear ch becomes progressively
simpler .
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The table below lists some data for spheres with radius of 2000, 1000,
500,
and
200
light years with l o 8 ,
lo7 , l o 6 ,
and l o 5 stars, respectively.
The data of the table have been derived along the lines indicated above.
Column gives the number of ar ea s to be scanned separately
i f
the survey
of the entire c eles tial sph ere is to be completed in one ye ar . The scanning
time fo r each a re a was assum ed approximately
10
t imes gre ater than the
figure given
in
column
4.
We s ee fr om the table that
if
th er e i s a single Earth-type civilization in
10
s ta rs , it s detection at the prese nt s tage of our technological development
s
nearly impossible;
i f
there
s
a sin gle civilization in
lo7
sta rs , i t can
be detected with some effort;
i f
there
s
one civilization in
lo6
s t a r s , i t s
detection by the available means s quite probable.
If the extraterrestrial civilization commands more powerful resources,
we can of course d etect it fro m considerably gre ate r distance s.
Once the existence of a civilization has been established, a larg e
antenna should be pointed in the corresp ondin g direction, since beside s the
powerful call signals intended fo r detection by other civilizations, it
probably transmits information, meaningful messages that can be picked
up with high-efficiency antennas only. To esta blish a bil ate ral communication,
we should send a radio m es sag e to the discovered civilization. Our signal
will be picked up without any difficulty, since our transmitter can be pointed
precisely in the direction of the ex tra ter re str ial civilization that we have
previous ly discove red. After th is prel imin ary exchange of m es sa ge s, the
antennas of the two civ ilizatio ns will be pointed a t one another and a m or e
effective exchange of in form ation will be es tabli shed .
In conclusion let us c on sid er the possibility of detecting a civilization
even though it does not tra ns m it special detection sign als. The power
of the radio tra ns m itte rs used for internal purposes by these civilizations
i s probably of the or der of ten s of kilowatts, and the antennas in common
4 S,
use have a directive gain g, -(the probab ility of picking up na rrow er
Z
antenna beams
s
too small) . The receive r passband, a s before, is
0.3
c / s .
A narrowe r passband
s
inadvisab le, sinc e the Doppler frequency shift will
not be compensated on the transm itting side. Fo r the sa me reaso n we
z ,
4
SI
take r=3 se c ,
P = 1 0 5
watt,--=lo,
S ,=105 , Y=70,Tn=30.
Fromequation
A ) ,
i
,
2
E
2
9 2
,
Q
P
2 2 5
s -
.Z
8
QJ
m
y:
2~
400m2
100m2
25 rn2
4 m 2
2000
1000
500
200
m
.
g
Z ' g S ,
~ 2 3
480,000
120,000
30.000
4,800
10'
10'
lo
10'
g
.g
Q
c QJ
m
2
E L
1
10
100
1000
10
ye rs
1
y e r
36
d ys
4
d ys
M g
.5
2
8 .Z
8
.g
480,000
12,000
300
5
*
2
36
d ys
4
d ys
9 hrs
1 hr
,
A
2 z
2
4 :
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R 3.1015mm, r 0.3 l ight ye ar s.
We se e that even the civi lizat ions occupying the nea res t s ta r s cannot be
detected unless they send special s ignals o r radiate (for some ob scure
rea so n) exceptionally high power.
O N L U S I O N S
If a civilization does not send sp ec ial detection1' sign als, i t apparently
cannot be detected even by i t s nea re st s te l la r neighbors.
If a civilization somew hat mo re advanced than we (app rox imate ly by a
few decades) sends spec ial radio signa ls, we can detect the se signa ls fr om
distan ces of 500-1000 light ye ar s.
Once civilizations have detected one another, they can establish radio
communicat ion on the galact ic scal e.