Fairey Fireflash

Fireflash
A Fireflash missile at the Royal Air Force Museum Cosford (2014)
Type	Air-to-air missile
Place of origin	United Kingdom
Service history
In service	1955–1958
Used by	United Kingdom
Wars	None
Production history
Designed	1949
Manufacturer	Fairey Aviation
No. built	c. 300
Specifications
Weight	150 kilograms (330 lb)
Length	111.75 inches (2,838 mm)
Detonation mechanism	Proximity fuze
Engine	Two solid fuel rocket motors
Wingspan	28.11 inches (714 mm)
Operational range	1.9 miles (3.1 km)
Speed	Mach 2 (max)
Guidance system	beam rider
Steering system	control surfaces
Launch platform	aircraft

Fireflash was the United Kingdom's first air-to-air guided missile to see service with the Royal Air Force. It was briefly deployed during the 1950s. Constructed by Fairey Aviation, the missile utilised radar beam riding guidance.

Produced in response to a Ministry of Supply requirement for a guided air-to-air missile, the project began in 1949 under the name Blue Sky. It was initially developed under the designation Pink Hawk. Blue Sky itself was a de-rated version of the Red Hawk missile.

About 300 missiles had been produced by 1955, but the Royal Air Force soon decided not to retain the type in its inventory. Many of the 300 missiles were expended in testing by 6 JSTU at RAF Valley and Woomera, South Australia from 1955–1957 using Meteor NF11 trials aircraft and subsequently by the Supermarine Swift fighters of No. 1 Guided Weapons Development Squadron at RAF Valley. The Fireflash was deployed on a very limited scale by the RAF in August 1957, and "had a limited capability against piston-engine bombers." The RAF deployed the later and more effective de Havilland Firestreak infra-red missile from August 1958.

The Fireflash was a beam riding missile - it was designed to fly down a radio beam emitted by the launch aircraft, which the pilot would keep aimed at the target.

It had a very unusual configuration: the missile body was unpowered. It was propelled by a pair of rocket boosters on the forward fuselage that were jettisoned 1.5 seconds after launch. The missile body, now travelling at around Mach 2, would coast the remaining distance to its target under guidance from the launch aircraft (the missile was unguided during the boost phase). The rocket engine nozzles were slightly offset to rotate the missile - this increased accuracy by evening out the effect of any slight asymmetry in thrust.