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Radar System Engineering

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724 RADAR RELAY [SEC. 17.14<br />

TaLE 17.1.—MAxIMuM RANGE OF RELAY SYSTEMS<br />

Frequency,<br />

Me/see<br />

Power,<br />

watts<br />

Beamwidth,<br />

9-ft<br />

paraboloid<br />

degrees<br />

3-ft<br />

paraboloid<br />

Free-space range, miles<br />

9-ft<br />

paraboloid<br />

3-ft<br />

paraboloid<br />

300<br />

1,000<br />

3,000<br />

10, OOO<br />

50<br />

25<br />

05<br />

01<br />

= 27<br />

8<br />

2.7<br />

0.8<br />

= 80<br />

24<br />

8<br />

2.4<br />

196<br />

460<br />

195<br />

292<br />

22<br />

,51<br />

22<br />

32.5<br />

When one considers the Dower involved, the decrease of man-made<br />

interference with increased frequency, and the privacy and protection<br />

from interference provided by narrow beams, microwave frequencies<br />

appear to be the most desirable. The decision between 3000 and 10,000<br />

Me/see was based largely upon the fact that in the latter case waveguide<br />

of a convenient size could be used, an extremely desirable design feature.<br />

Since a 32-mile range is adequate for the uses intended, and since too<br />

great sharpness of beam might lead to alignment difficulties, 3-ft paraboloids<br />

were used at both stations.<br />

Frequency modulation was chosen, partly because of its advantages<br />

when signal-to-noise and signal-to-interference ratios are high, but mostly<br />

because it simplified the oscillator design. Large deviations of the oscillator<br />

are easily accomplished, and there are no problems of r-f bandwidth.<br />

Since the required video bandwidth was about 1.5 Me/see, a total<br />

deviation of 6 Jfc/sec was chosen. The total frequency spectrum<br />

involved is then a little more than 9 hlc/sec. In order to minimize the<br />

required i-f bandwidth in the receiver, the discriminator was set on one<br />

side of the pass band of the receiver. A value of 11 31c/sec was then<br />

chosen for the i-f bandwidth to provide a margin to take care of improper<br />

tuning.<br />

The equipment is shown schematically in Fig. 17”19. The oscillator, a<br />

2K39 reflex klystron, is stabilized against a cavity by means of a microwave<br />

discriminator. 1 The output of this device is a d-c signal whose ~’oltage is<br />

proportional to the deviation of the oscillator frequency from the frequency<br />

for which a resonant cavity, used as comparison standard, is set.<br />

This error signal is amplified by a push-pull d-c amplifier and used to<br />

control the reflector voltage of the klystron in such a way that its frequency<br />

is forced into agreement with the resonant frequency of the cavity.<br />

l~ideo signals and pulses are applied directly to the reflector to produce<br />

the desired frequency modulation. Rapid response is purposely avoided<br />

I R. V. Pound, A Microwave Frequency Discriminator, RL Report No. 662,<br />

Aug. 4, 1945; Reu: Sci. InSt. 17, 490 (1946).

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