![]() Front-oblique view of the AN/APS-4 radar pod without its external shell | |
Country of origin | UK |
---|---|
Introduced | 1943 |
Type | Surface-search radar |
Frequency | 3300 ±50 MHz (S-band) |
PRF | 660 pps |
Beamwidth | ~10º horizontal, ~15º vertical |
Pulsewidth | 1 μs |
RPM | 60 rpm |
Range | 1 to 100 miles (1.6–160.9 km) |
Diameter | 28 in (0.71 m) |
Azimuth | 320º |
Precision | ~5º |
Power | 40 kW |
Other names | ASH, PS-18/A |
Related | AN/APS-5, AN/APS-6 |
The AN/APS-4, originally known as ASH (air-surface, model H) is an early military air-to-air and air-to-surface radar used by American and British warplanes during World War II.
APS-4 operated in the X band at 3 cm, compared to the 10 cm S band used by most radars of the era. This allowed the antenna to be greatly reduced in size and the unit as a whole to fit into a single streamlined fairing that could be mounted to many aircraft.
In American service it was used on many aircraft, including the Douglas C-47 Skytrain, North American P-82D/F/H Twin Mustang, Vought F4U-2\5N Corsair, Grumman F6F-3/5 Hellcat, Curtiss SB2C-5 Helldiver and Grumman TBF-3 and TBM-3S Avenger, and Curtiss SC Seahawk.
In Fleet Air Arm and RAF service it was known as ASV Mark IX and equipped a number of aircraft including the Fairey Firefly, Fairey Barracuda, de Havilland Mosquito and a small number of Grumman Avengers.
In service of the Swedish Air Force, it was known as PS-18/A and was equipped on the Saab 18, primarily on the reconnaissance version, S 18A but it was also used on the bomber and torpedo versions B 18A, B 18B, and T 18B. [1] The PS-18/A had slightly improved maritime performance: the beacon navigation function was disabled, and a sea clutter filter, a simple, switchable shortened time constant in the video chain, was introduced. [2]
The APS-4 radar is a lightweight air-to-air and air-to-surface radar with a detection range for large ships of about 15 miles (24 km), and about 5 miles (8.0 km) against aircraft. It could also detect coastline at approximately 75 miles (121 km). [3]
Physically, the APS-4 consists of a control box, one or two indicators, the same number of indicator-amplifiers, an antenna, a transmitter-receiver, and a cable junction box. [4] The antenna and transmitter-receiver were typically housed externally below one wing, in a fiberglass shape that was similar to a Mk 17 500-pound (230 kg) bomb. [5] These displays could be set for ranges of 4, 20, 50, and 100 nautical miles (6, 30, 80, and 160 km). [6] The radar weighed 180 pounds (82 kg). [6]
The APS-4 broadcast in the X-band with a wavelength of 3 cm. [6] [4] Peak broadcast power varied from 40 to 70 kW according to radar version. Pulse repetition frequency was adjustable by the operator to either 600 or 1000 pulses per second. [7]
The APS-4 emitted a radio beam in the form of a 6° cone. The beam could be directed in three modes, manual, search and intercept. In manual mode the beam was aimed by operator control from 10° above, to 30° below the longitudinal axis of the aircraft. In search mode, the radar beam scans through 150° in azimuth, and while doing so would run two lines scans, each separated by 4°. This caused the beam to cover 10° in a vertical plane. In intercept mode, the beam executes a four-line scan, with 6° between lines, to cover a vertical plane of 24°. [5] Results were displayed on one or two 3-inch displays. [4]
An improved version was called the AN/APS-5. A simplified version for single-seat fighters was called the APS-6. [8]