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Project Cyclops, A Design... - Department of Earth and Planetary ...

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practical limits <strong>of</strong> narrow beamwidths in the microwave<br />

region as well, the photon energy disadvantage shows<br />

through. But there are additional specific disadvantages<br />

that are revealed by each <strong>of</strong> the laser systems studied.<br />

Optical system A suffers from too little energy per bit. If<br />

its pulse energy were equal to that <strong>of</strong> the other systems,<br />

its range would increase over 10 times. Optical system B<br />

does not adequately override star noise, so about 30<br />

times as many signal photons must be received per pulse<br />

as for optical system A <strong>and</strong>, because <strong>of</strong> the filter loss,<br />

the received energy per pulse is only 25 times as great at<br />

the same range. Infrared system A suffers from the<br />

inefficient array utilization because <strong>of</strong> incoherent addition<br />

<strong>and</strong> the spontaneous emission noise associated with<br />

each receiver. Finally, infrared system B suffers from the<br />

small size <strong>of</strong> receiving antenna possible in a coherent<br />

system<br />

at 10.6/a.<br />

Except possibly for infrared system B, all the laser<br />

systems would appear to be far more expensive than<br />

microwave A. Certainly to provide two acres worth <strong>of</strong><br />

optical collecting area in the form <strong>of</strong> precisely steerable<br />

2- to 5-m telescopes would cost much more than a single<br />

l O0-m dish. All the systems require cooled detectors.<br />

Optical B requires costly precision narrow b<strong>and</strong> filters at<br />

each antenna. Infrared A requires precision local lasers<br />

<strong>and</strong> mixers at each <strong>of</strong> 1975 antennas, while the precision<br />

needed for the local oscilla{or <strong>of</strong> infrared B may be<br />

beyond the capabilities <strong>of</strong> even the most advanced<br />

technology.<br />

The mechanical stability <strong>and</strong> precision problems <strong>of</strong><br />

the laser systems have their counterpart in the precision<br />

<strong>of</strong> electrical control needed to compensate for Doppler<br />

drifts. The drift due to <strong>Earth</strong> diurnal Doppler could be<br />

as great as 3 kHz/sec at 10.6/,( for stars near tile meridian<br />

<strong>and</strong> a station near the equator. Locking infrared system<br />

B onto such a rapidly drifting signal would be a<br />

nightmare. The total interstellar Doppler shift is about<br />

_+10-3 so the filters in the optical systems would require<br />

tunability over a +-300 GHz range while the infrared<br />

systems would need a -+30 GHz tuning range.<br />

Finally, laser systems suffer from atmospheric absorption<br />

even in clear weather <strong>and</strong> are unusable in cloudy<br />

weather. Sky light does not materially affect the<br />

performance <strong>of</strong> any <strong>of</strong> the systems, except for optical<br />

system B. In the daytime, the background count from<br />

the sky would reduce the range <strong>of</strong> this system from 24<br />

to about 20 light-years. Thus all systems would be usable<br />

in clear daytime hours as well as at night, but the<br />

microwave systems are the only all-weather systems.<br />

In summary<br />

1. The sole advantage <strong>of</strong> lasers is that they permit<br />

narrow beamwidths to be realized with small<br />

transmitting mirrors, but this advantage turns into<br />

a disadvantage at the receiver where we need a<br />

large collecting<br />

area.<br />

2. The collecting surface is much cheaper <strong>and</strong> more<br />

durable in the microwave region, because the<br />

tolerances are much greater <strong>and</strong> polished surfaces<br />

are not needed.<br />

3. Microwave systems <strong>of</strong>fer substantially more range<br />

for the same power, even with wider beamwidths.<br />

4. Because <strong>of</strong> the wider beams, automatic positioning<br />

<strong>and</strong> tracking are feasible at microwaves on a dead<br />

reckoning basis.<br />

5. Doppler shifts <strong>and</strong> drift rates are orders <strong>of</strong><br />

magnitude less at microwave frequencies <strong>and</strong> can<br />

easily<br />

be compensated.<br />

6. Microwave systems are all-weather systems.<br />

We have gone to some length to compare microwaves<br />

<strong>and</strong> lasers because the ease <strong>of</strong> obtaining sharp beams has<br />

led many people to propose laser systems (ref. 3). We<br />

have made the comparison for point-to-point communication<br />

links where the transmitting directivity <strong>of</strong> the<br />

laser is used. When we come to consider the search<br />

problem in the next chapter we will see that transmitter<br />

directivity is not an asset, <strong>and</strong> lasers lose out completely.<br />

In fact, we believe that if lasers had been known for the<br />

last hundred years <strong>and</strong> microwaves had only recently<br />

been discovered, microwaves would be hailed as the long<br />

sought for answer to interstellar communication.<br />

COMMUNICATION RATE OF A MICROWAVE LINK<br />

At the range limits given, the links compared in the<br />

last section are all 1 bit/sec systems with a bit error rate<br />

<strong>of</strong> 0.07865. As long as the received energy per bit is held<br />

constant, the error rate will not change. Thus the<br />

connnunication rate varies inversely as the square <strong>of</strong> the<br />

_,<br />

,ookw7s,_o-_ / / / gi/ .-ry<br />

F 2ookw2._,,o -2 / / /._'/.-"/7<br />

Lmlk<br />

I I01 10 2 10 3 10 4 I0 5<br />

CLEAR APERTURE DIAMETER, m<br />

FigureS-8. Information rates <strong>of</strong> microwave links;<br />

X = 3 cm.<br />

51

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