Missile Red Top

Summary

CategoryAir-to-Air Missiles
Sub-typeAir-to-air missile
Origin country πŸ‡¬πŸ‡§ United Kingdom
ManufacturerHawker Siddeley
StatusRetired
Year of service1964

Technical specifications

WarheadExpanding-rod
Warhead weight31 kg (68 lb)
Diameter230 mm (9.1 in)
Span910 mm (35.8 in)
Length3,320 mm (130.7 in)
Weight154 kg (340 lb)
Range 18 km (11 mi)
Max. speed3,920 km/h (Mach 3.9)

Red Top scale diagram

Red Top β€” Air-to-Air 1.75 m 3.32 m
Range
18 km
Speed
Mach 3.9
Weight
154 kg
Warhead
31 kg

Operators

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

Carried by

Description

The Red Top was the third indigenous British air-to-air missile to enter service, succeeding the Firestreak and Fireflash. Developed from the "Blue Vesta" project initiated to counter supersonic bombers, the missile program was designated Red Top in November 1957. The design aimed to provide a head-on, all-aspect interception capability. Flight testing began with aerodynamic test vehicles in 1959, followed by guidance trials from a Canberra in 1960, and launches from a Lightning in 1961. The missile entered service in 1964.

The missile utilized infrared homing guided by an indium antimonide seeker. This seeker allowed head-on engagements against supersonic targets heated by skin friction, though subsonic targets required a tail-aspect approach. The seeker featured an expanded field of view compared to its predecessor. Red Top transitioned from vacuum-tube electronics to transistorized systems, eliminating the need for an aircraft-mounted ammonia cooling system and utilizing highly filtered air instead.

The internal layout featured a straightened fuselage. The warhead was moved forward, allowing the control actuators and their powering air bottle to be positioned directly at the rear fins. This rearrangement allowed for a larger rocket motor. The missile carried an expanding-rod warhead, which was larger than the blast-fragmentation warhead of the Firestreak. It utilized an infrared proximity fuse with rectangular windows. Due to its infrared guidance system, the missile could only be launched outside of cloud cover.

The Red Top was operated by the United Kingdom (Royal Air Force and Royal Navy Fleet Air Arm), Kuwait, and Saudi Arabia. In British service, it was deployed on the Sea Vixen and the Lightning. Carrying the missile on the Lightning required modifications to the aircraft's vertical stabilizer to maintain stability at high speeds; consequently, older Lightning models continued to carry the Firestreak. The Red Top remained in service until 1988, when it was retired alongside the remaining Lightning fleet. It was also evaluated but rejected for use on the Phantom due to integration costs and weight considerations.

Frequently Asked Questions

What type of missile is the Red Top?
The Red Top is an air-to-air missile developed by the United Kingdom. It entered service in 1964.
What is the range of the Red Top?
The Red Top has a maximum range of approximately 18 km (11 miles). Effective range varies with launch platform, altitude, and flight profile.
How fast is the Red Top?
The Red Top reaches a maximum speed of 3,920 km/h (Mach 3.2).
What warhead does the Red Top carry?
The Red Top carries a expanding-rod warhead weighing 31 kg.
How is the Red Top guided?
The Red Top uses infrared homing guidance.
Which countries use the Red Top?
The Red Top is in service with 3 countries: United Kingdom, Kuwait, Saudi Arabia.
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