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Radar System Engineering

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22 THE RADAR EQUATION [SEC.25<br />

Again we call attention to the fact that Eq. (3b), like Eq. (2), contains G<br />

rather than Go, and is not restricted to any particular direction or to<br />

beams of any special shape. The sole restriction which has not yet been<br />

made explicit is that G should not vary significantly over the angle which<br />

the target subtends at the radar antenna.<br />

Usually we shall be interested in the signal that is returned when the<br />

target lies somewhere along the maximum of the radar beam, and we<br />

should then replace G by G,. It is instructive to proceed then to eliminate<br />

GOby means of Eq. (l), obtaining<br />

S = P(TA ‘j2<br />

47rR%2”<br />

(4a)<br />

Note that AZnow appears in the denominator, while the numerator contains<br />

the square of the area of the antenna aperture. A further manipulation<br />

of Eq. (4a) is of interest. Suppose the minimum power required<br />

for satisfactory detection, Smin, is known; we may solve Eq. (4a) for the<br />

maximum range of detection, R~..:<br />

4 PuA ‘jz<br />

R .s, = — (4b)<br />

J 4~S~,.A2”<br />

At this point it may be well to get an idea of the order of magnitude<br />

of the quantities involved by inserting numbers not unusual in wartime<br />

pulse-radar practice. If we choose X = 0.10 ft ( = 3.0 cm), P = 10’<br />

watts, A = 10 ft 2, j = 0.6, u = 100 ftz (typical for small aircraft),<br />

& = 5 X 10–12 watts, we obtain R~.. = 155,000 ft or 29 statute miles.<br />

We observe that a 16-fold increase in transmitted power is required to<br />

double the maximum range; on the other hand, it would appear that R~..<br />

could be doubled by doubling the linear dimensions of the antenna. But<br />

the latter step would at the same time reduce the beamwidth by a factor<br />

of 2 and as we shall see in Sec. 2“11 that this indirectly affects Sti.. A<br />

change in wavelength is even more difficult to discuss as it entails changes<br />

in S~i., P, and possibly u as well.<br />

2.5. Beams of Special Shapes.—In several applications of radar, use<br />

is made of an antenna designed to spread the radiated energy out over a<br />

considerable range in angle in one plane. The object usually is to<br />

increase the angular region covered at one time. An example of such a<br />

radiation pattern is the simple “fan beam” sketched in Fig. 2.1. It is<br />

easy to produce such a beam by means of an antenna whose effective<br />

aperture is wide in the direction in which the beam is to be narrow and<br />

narrow in the direction in which the beam is to be broad. The connection<br />

given by Eq. (1) between aperture and gain still holds, implying<br />

that by reducing the vertical dimension of the antenna aperture (in<br />

Fig. 2.1), gain has necessarily been sacrificed; of course this is inevitable,

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