KA3N Gorgon III
The Gorgon III – given the military designations KA3N, KU3N, CTV-N-6 and RTV-N-4 – was a rocket-powered air-to-air missile developed by the United States Navy near the end of World War II. With the end of the war, the program was changed to that of a research vehicle for missile control systems; both single and twin-rocket-powered versions were built and tested.
Design and development
The Gorgon missile program began in July 1943 at the Naval Aircraft Modification Unit in Warminster, Pennsylvania, and was intended to develop a family of small air-launched missiles for air-to-air and air-to-surface roles. The Gorgon III was intended as an air-to-air missile for use by patrol aircraft; it would have a conventional aircraft-type design, with a high-mounted wing and twin tail fins. Originally three different propulsion systems were to be trialed; Gorgon IIIA was to be rocket-powered; Gorgon IIIB powered by a turbojet engine, and Gorgon IIIC was to use pulsejet propulsion; however Gorgon IIIC was later changed to a rocket-powered configuration. Both Gorgon IIIA and, in its as-built configuration, Gorgon IIIC were to be powered by the Reaction Motors CLM2N liquid-fuel rocket, fueled with monoethylamine and nitric acid, with a single motor in the IIIA and twin motors in the Gorgon IIIC. Guidance was to be provided by a combination of television guidance, the missile steered by radio command from the launching aircraft to the target via a camera in the nose of the missile, with a backup seeker head of unspecified type.In April 1945, orders had been placed for 34 Gorgon IIIA missiles, with 16 Gorgon IIIBs and 20 Gorgon IIICs also on contract. However, the guidance system had proved to be unworkable in tests of the Gorgon IIA missile, and with the end of the war the program was realigned as a pure testing effort for missile control and guidance systems.