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Radar System Engineering

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20 THE RADAR EQUATION [SEC.22<br />

radiate a well-defined beam. This maximum value of G we shall denote<br />

by GO. The narrow, concentrated beams which are characteristic of<br />

microwave radar require, for their formation, antennas large compared<br />

to a wavelength. In nearly every case the radiating system amounts to<br />

an aperture of large area over which a substantially plane wave is excited.<br />

For such a system, a fundamental relation connects the maximum gain<br />

G,, the area of the aperture A, and the wavelength:<br />

(1)<br />

The dimensionless factor .f is equal to 1 if the excitation is uniform in<br />

phase and intensity over the whole aperture; in actual antennas f is often<br />

as large as 0.6 or 0.7 and is rarely less than 0.5. An antenna formed by a<br />

paraboloidal mirror 100 cm in diameter, for a wavelength of 10 cm,<br />

would have a gain of 986 according to Eq. (1) with ~ = 1, and in practice<br />

might be designed to attain GO = 640.<br />

The connection between gain and beamwidth is easily seen. Using<br />

an aperture of dimensions d in both directions, a beam may be formed<br />

whose angular width, 1 determined by diffraction, is about X/d radians.<br />

The radiated power is then mainly concentrated in a solid angle of X2/dZ.<br />

An isotropic radiator would spread the same power over a solid angle<br />

of 4T. Therefore, we expect the gain to be approximately 4rd2/X’, which<br />

is consistent with Eq. (1), since the area of the aperture is about d’. For<br />

a more rigorous discussion of these questions the reader is referred to<br />

Vol. 12, Chap. 5.<br />

A complementary property of an antenna which is of importance<br />

equal to that of the gain is the e.fective receiving cross section. This<br />

quantity has the dimensions of an area, and when multiplied by the power<br />

density (power per unit area) of an incident plane wave yields the total<br />

signal power available at the terminals of the antenna. The effective<br />

receiving cross section A, is related to the gain as follows:<br />

A . G@2.<br />

,<br />

4rr<br />

Note that G, not Go, has been written in Eq. (2), the applicability of<br />

which is not restricted to the direction of maximum gain or to beams of<br />

any special shape. Once the gain of the antenna in a particular direction<br />

is specified, its effective receiving cross section for plane waves incident<br />

jrom that direction is fixed. Equation (2) can be based rigorously on the<br />

Reciprocity Theorem (see Vol. 12, Chap. 1). Comparing Eqs. (2) and<br />

(1) we observe that, if the factor j is unity, the effective receiving cross<br />

1Wherever a precise definition of beamwidth is intended, we shall mean the<br />

angularintervalbetweentwo directionsfor whichG = G,/2.<br />

(2)

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