Missile Firestreak

Summary

CategoryAir-to-Air Missiles
Sub-typeAir-to-air missile
Origin country πŸ‡¬πŸ‡§ United Kingdom
Manufacturerde Havilland Propellers
StatusRetired
Year of service1957

Technical specifications

WarheadAnnular blast fragmentation
Warhead weight23 kg (50 lb)
Diameter223 mm (8.8 in)
Span750 mm (29.5 in)
Length3,190 mm (125.6 in)
Weight136 kg (300 lb)
Range 6.4 km (4.0 mi)
Max. speed3,675 km/h (Mach 3.7)

Firestreak scale diagram

Firestreak β€” Air-to-Air 1.75 m 3.19 m
Range
6.4 km
Speed
Mach 3.7
Weight
136 kg
Warhead
23 kg

Operators

πŸ‡¬πŸ‡§ United Kingdom • πŸ‡°πŸ‡Ό Kuwait • πŸ‡ΈπŸ‡¦ Saudi Arabia

Carried by

Description

The Firestreak was a British first-generation, passive infrared homing air-to-air missile. Developed in the early 1950s under the rainbow code "Blue Jay," the project originated from requirements for a tail-aspect weapon. The first airborne test launch occurred in 1954 from a Venom aircraft, destroying a target drone. The missile entered active service in 1957.

The weapon operated as a rear-aspect, fire-and-forget pursuit missile. Guidance was provided by a lead telluride infrared seeker protected by an eight-faceted conical arsenic trisulphide nose designed to prevent ice accretion. The seeker was cooled to extremely low temperatures using an ammonia-cooled heat exchanger. Because the vacuum-tube electronics generated heat, the missile required external cooling from the launch aircraft prior to takeoff, as well as heated air from the aircraft's engine compressor to prevent moving parts from freezing before launch. Internally, the electronics occupied the forward fuselage, requiring the blast-fragmentation warhead to be positioned at the rear, wrapped around the rocket nozzle. Consequently, the actuators for the rear control fins were mounted in the nose and connected via long pushrods. The solid-fuel rocket motor was positioned in the center of the fuselage. The warhead was triggered by optical proximity fuzes behind windows in the forward fuselage or by contact fuzes on the wings, dispersing fragments forward upon detonation. To launch the weapon, the seeker was slaved to the radar of the host aircraft until acquiring a lock. The missile could only be fired in clear conditions outside of clouds, and ground crew required protective gear during handling due to toxicity from the motor or coolant.

The missile was operated by the United Kingdom's Royal Air Force and Fleet Air Arm, the Kuwait Air Force, and the Royal Saudi Air Force. It equipped the Lightning interceptor, Sea Vixen naval fighter, and Javelin all-weather interceptor. Although a successor missile, the Red Top, entered service in 1964, the Firestreak remained in service with the Royal Air Force until 1988. This prolonged service occurred because older models of the Lightning interceptor lacked the vertical tail area required to stabilize the larger wings of the successor missile.

Frequently Asked Questions

What type of missile is the Firestreak?
The Firestreak is an air-to-air missile developed by the United Kingdom. It entered service in 1957.
What is the range of the Firestreak?
The Firestreak has a maximum range of approximately 6.4 km (4.0 miles). Effective range varies with launch platform, altitude, and flight profile.
How fast is the Firestreak?
The Firestreak reaches a maximum speed of 3,675 km/h (Mach 3.0).
What warhead does the Firestreak carry?
The Firestreak carries a annular blast fragmentation warhead weighing 22 kg.
How is the Firestreak guided?
The Firestreak uses rear-aspect infrared homing guidance.
Which countries use the Firestreak?
The Firestreak is in service with 3 countries: United Kingdom, Kuwait, Saudi Arabia.
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