RIM-50 Typhon LR | |
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Test Launch of Development Missile
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|
Type | Long range surface-to-air missile |
Place of origin | United States |
Service history | |
In service | Canceled December 1963 |
Used by | United States Navy |
Production history | |
Manufacturer | Bendix |
Specifications | |
Weight | 2,060 pounds (937 kg) |
Length | 15.5 feet (4.70 m) |
Diameter | 1.5 feet (0.47 m) |
Warhead | High explosive 150 pounds (68 kg) continuous rod, blast fragmentation or W-60 low-yield nuclear warhead |
Detonation
mechanism |
Proximity Fuse |
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|
Engine | Two-stage, Solid-fueled rocket booster; ramjet sustainer |
Wingspan | 5.15 feet (1.57 m) |
Propellant | Solid fuel |
Operational
range |
200 nm (370 km) |
Flight ceiling | 95,000 feet (29,000 m) |
Speed | Mach 4.0 |
Guidance
system |
Inertial |
Launch
platform |
Ship |
The RIM-50 Typhon LR was a missile that was intended to be a Terrier missile–sized replacement to the Talos missile to be used with the Typhon combat system. The RIM-50 was canceled in 1963 along with the medium range RIM-55, when the Typhon combat system was canceled. The technology in development for this missile was incorporated into the RIM-67 Standard missile.