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Radar System Engineering

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180 THE GATHERING AND PRESENTATION OF RADAR DATA [%C. 69<br />

were large gaps in its vertical coverage (Figs. 6.14 and 615). The range<br />

on low-flying aircraft was poor. The system was supplemented in 1940<br />

by 200-Mc/sec equipment, the so-called “ CHL” (Chain, Home, Low)<br />

system. It was often very difficult to find sites that were flat enough<br />

for stations. Since the station at Dover was on a 400-ft cliff and Ventnor<br />

was on a cliff 1000 ft above the sea, it was im~ossible for these stations to<br />

measure height at all. The processes involved in deducing the plan position<br />

and. the height of an aircraft were complicated and not very reliable.<br />

The maximum traffic-handling capacity was low (a good operator could<br />

pass about 6 plots per minute), and the system could not keep track of<br />

large numbers of independently routed aircraft. Nevertheless, formations<br />

of aircraft were plotted reliably, and the number of aircraft in h<br />

formation could be estimated by an experienced operator. With all its<br />

imperfections, this s’ystem was the basis of the British radar defense for<br />

the greater part of the war.<br />

!!’he CXAM.—While the British Home Chain was being designed and<br />

installed, the Army and Navy development agencies in the United States<br />

were independently developing pulse radar equipment. The earliest<br />

service equipment to be commercially manufactured was the CXAM<br />

radar, designed at the Naval Research Laboratory. A laboratory-built<br />

prototype of this set tvas tested at sea during battle maneuvers in early<br />

1939, aboard the U.S.S. New York, and its performance was so promising<br />

that a contract was let in October 1939 for the manufacture of six sets of<br />

similar equipment.<br />

The CXAM was operationally quite different from the CH. Instead<br />

of using separate, fixed, broad-beam transmitting and receiving arrays,<br />

it employed a common antenna for transmitting and receiving. To produce<br />

as narrow as beam as possible, it operated at the then ultrahigh<br />

frequency of 195 Me/see, and employed a “mattress” array of dipoles<br />

with reflectors, giving a gain of 40 and a beam 14° wide in azimuth by<br />

about 70° in elevation. The antenna could be rotated in azimuth at a<br />

speed of 5 rpm, or manually trained to follow a particular target. The<br />

peak pulse power was 15 kw, the pulsewidth 3 psec, and the repetition<br />

rate 1640 pps. Range against bombers was about 70 miles, against<br />

fighters about 50 miles.<br />

The display was an A-scope in which the trace was lengthened by<br />

causing the sweep to take place from left to right across the tube, then<br />

drop down and return from right to lem Range was estimated with the<br />

help of marks on the face of the tube; bearing was determined as<br />

the direction of antenna-pointing which yielded maximum signal. The<br />

height of targets could be estimated with the help of nulls in the vertical<br />

antenna pattern (Sec. 611).<br />

Despite its early design and its lack of adequate coverage against low-

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