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Radar System Engineering

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46 THE RADAR EQUATION [SEC.211<br />

Although we have not arrived at a universal prescription for the<br />

minimum detectable signal power, we have studied the influence of<br />

various factors onS~i~, and weare nowin a position to predict therelutive<br />

change in &i. which will accompany some proposed alteration in the<br />

radar system. Onewayto establish some absolute basis isto give the<br />

~bserved value of the ratio of minimum detectable signal power to<br />

average noise power, for one particular system. This is done in Table<br />

22, in which are displayed the relevant constants of the system selected.<br />

TABLE 22.-(2HARACTERISTICS OF A SAMPLE SYSTEM<br />

Type of indication.<br />

PPI; P7 screen;decay time about 7 sec<br />

I-f bandwidth. . . . . . . . . . . . . . . . . @=l.2Mc/sec<br />

Video bandwidth.,.... ., b = 5 Me/see<br />

Pulseduration. . . . . . . . . . . . . . . . T=l.Oxee<br />

Pulserepetitionfrequency. 320 pps Hence about 50 pulses on one point<br />

Scan rate..................,., 6rpm targetperscan, with negligiblescan-<br />

Beamwidth. . . . . . . . . . . . . . . . . . . 0=6° ) to-scan storage.<br />

Sweepspeed. . . . . . . . . . . . . . . . . . v=2X10’cm/sec Note that d/u> r, which is<br />

Spot diameter. . . . . . . . . . . . . . . . d= O.lcm<br />

not the best condition, but<br />

} is a typical one.<br />

conditions of observation. Signal occurs on one scan, at known azimuth, in<br />

one of six rangepositions. Observermust locate<br />

it with 90% certainty. This corresponds to a<br />

value of rv,in Table 2.1, of the orderof 10–1,<br />

Ratio of minimum detectabk signal<br />

power to average nm”se<br />

power, under above cmditiom. 1,25 (+1 db)<br />

Working from Table 2.2, we can infer that if the system there described<br />

had an over-all noise figure N of, for example, 15, the signal power required<br />

at the terminals of the antenna would be S~im= 1.25NkT@ = (1.25) (15)<br />

(1.37 X 10-23) (291) (1.2 X 10’) = 9 X 10-’4 watts. Now if for some<br />

other system N is given, together with the new values of the parameters<br />

listed in Table 2.2, the reader should be able to estimate Stim for that<br />

system. The estimate will be better, of course, the less extreme the<br />

departure from the conditions of Table 2.2. We must emphasize, however,<br />

the limited utility of a value of Sti. obtained in this way. The<br />

experiments upon which Table 2.2 is based were performed in the laboratory<br />

under ideal conditions of observation; moreover, the value of w (the<br />

parameter of Table 21) is here certainly much too large for any radar<br />

search operation, although it might not be inappropriate for the continuous<br />

tracking of a target already detected.<br />

The experimental determination of the maximum range of an actual<br />

radar set is as uncertain a matter as is the calculation of the maximum<br />

range by the method outlined in this chapter. Some arbitrary procedure<br />

for observation must be specified, and the limit of range must be defined

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