Firestreak | |
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A Firestreak being prepared for loading onto a Lightning, RAF Akrotiri, December 1963
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Type | air-to-air missile |
Place of origin | United Kingdom |
Service history | |
In service | 1957–1988 |
Used by | United Kingdom, Kuwait, Saudi Arabia. |
Production history | |
Designed | 1951 |
Manufacturer | de Havilland Propellers |
Specifications | |
Weight | 136 kg (300 lb) |
Length | 3.19 metres (10 ft 6 in) |
Diameter | 0.223 m (8.8 in) |
Warhead | 22.7 kg (50 lb) annular blast fragmentation |
Detonation
mechanism |
proximity infrared |
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Engine | Magpie solid fuel motor |
Wingspan | 0.75 m (30 in) |
Operational
range |
4 miles (6.4 km) |
Speed | Mach 3 |
Guidance
system |
rear-aspect infrared |
Steering
system |
control surface |
Launch
platform |
fixed-wing aircraft |
The de Havilland Firestreak is a British first-generation, passive infrared homing (heat seeking) air-to-air missile. It was developed by de Havilland Propellers (later Hawker Siddeley) in the early 1950s and was the first such weapon to enter active service with the Royal Air Force (RAF) and Fleet Air Arm, equipping the English Electric Lightning, de Havilland Sea Vixen and Gloster Javelin. It was a rear-aspect, fire and forget pursuit weapon, with a field of attack of 20 degrees either side of the target.
The Firestreak was the third heat seeking missile to enter service, after the AIM-4 Falcon and AIM-9 Sidewinder which both entered service the previous year. In comparison to those designs, the Firestreak was much larger and heavier, carrying a much larger warhead. It had otherwise similar performance in terms of speed and range. Limitations of the design led to an improved version, the Hawker Siddeley Red Top, but this never completely replaced Firestreak. Firestreak remained in service until 1988, when it was retired along with the last RAF Lightnings.
Firestreak was the result of a series of projects begun with the OR.1056 Red Hawk missile. When this proved too ambitious for the then state of the art, a lower performance specification was released in 1951 as OR.1117, and given the Ministry of Supply rainbow codename Blue Jay.
Blue Jay developed as a fairly conventional-looking missile with cropped delta wings mounted just aft of the midpoint and small rectangular control surfaces in tandem towards the rear. Internally, things were considerably more complex. The rear-mounted controls were operated by nose-mounted actuators via long pushrods. The actuators were powered by compressed air from bottles at the rear. The lead telluride (PbTe) IR seeker was mounted under an eight-faceted conical arsenic trisulphide "pencil" nose and was cooled to −180 °C (−292.0 °F) by anhydrous ammonia to improve the signal to noise ratio. The unusual faceted nose was chosen when a more conventional hemispherical nose proved prone to ice accretion. There were two rows of triangular windows in bands around the forward fuselage, behind which sat the optical proximity fuzes for the warhead. The warhead was at the rear of the missile, wrapped around the exhaust of the Magpie rocket.