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Radar System Engineering

Radar System Engineering

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SEC. 10.5] MAGNETRON CHARACTERISTICS 351<br />

promise between efficiency and frequency stability and this compromise<br />

is arrived at from a study of the Rieke diagram.<br />

It is possible in some cases to combine with the magnetron proper a<br />

high-Q cavity coupled to it in such a way as to reduce the pulling figure<br />

by a large amount with little or no loss in efficiency. The ratio of the<br />

pulling figures with and without the high-Q cavity for equivalent operating<br />

conditions is called the “stabilization factor, ” which may be as large<br />

as 10 but is usually between 2 and 5. The addition of this stabilizing<br />

!0<br />

.0<br />

)<br />

FIG. 10.24.—Characteristicsof the 4J70 series.<br />

Magnetic field = 2700gauss<br />

Pulse current = 70 amp<br />

Pulse duration = 0.8psec<br />

PRF = 400ppS.<br />

cavity has the disadvantage, however, of reducing the tuning range of<br />

the magnetron; further, it may aggravate mode instabilities. If constant-frequency<br />

operation is required, stabilized magnetrons should be<br />

seriously considered.<br />

Frequency stabilization has been incorporated into only a few magnetrons.<br />

A good example is the 2J41, which has a pulse power output of<br />

500 watts at 9310 Me/see and a pulling figure of 1.5 Me/see with a<br />

tuning range of 0.7 per cent. The stabilization factor is 10. The 10-cm<br />

series 4J70 to 4J77 is stabilized by a factor of 1.5 and the 1.25-cm 3J21<br />

by a factor of 2. High-power magnetrons with high stabilization have<br />

not been deveIoped.<br />

Weight.—The development of airborne radar placed great emphasis<br />

on the reduction in weight of all components. As a result, magnetronmagnet<br />

combinations were produced in which every effort was made to<br />

reduce the total weight. This development has been so successful, particularly<br />

for the higher-frequency magnetrons, that the weight of a

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