AN/APS-20
Description of the radar set, tactical-technical characteristics

Figure 1: AN/APS-20 fitted to the TBM-3W

General Electric
Specifications | |
---|---|
frequency: | 2 860 … 2 880 MHz
(S-Band) |
pulse repetition time (PRT): | |
pulse repetition frequency (PRF): | 300 Hz |
pulsewidth (τ): | 2 µs |
receiving time: | |
dead time: | |
peak power: | 1 MW |
average power: | |
instrumented range: | 250 NM (≙ 460 km) |
range resolution: | |
accuracy: | |
beamwidth: | |
hits per scan: | |
antenna rotation: | 6 or 3 min⁻¹ |
MTBCF: | |
MTTR: |
AN/APS-20
The AN/APS-20 was an operating in S-Band surface search radar for airborne early warning (AEW). It was complemented by the AN/APX-13 Identification Friend of Foe (IFF) system.
The transmitter used a magnetron. The AN/APS-20 has a number of special circuits for the suppression of Seeclutter and other sources of noise. The IF-frequency was 30 MHz with a bandwidth of 1.5 MHz and an amplifier noise figure of 2.5 dB. It had a PPI scope with a 12 inch cathode ray tube with a long-persistence phosphor. The eight-foot antenna was installed in a large circular radome mounted in the underbelly position just behind the nose wheeldoors.
The AN/APS-20 was initially developed during WWII but did not enter operational service until 1946. The radar as fitted to the TBM-3W and PB-1W became the mainstay of AEW aircraft developments following World War Two. Modifications were AN/APS-20B, AN/APS-20E, and AN/APS-20F with up to 2 MW pulse power. AN/APS-20 was replaced since 1956 by the AN/APS-95 and AN/APS-103 but some sets were operational up to 1978.