RIM-50 Typhon
RIM-50 Typhon LR | |
---|---|
Test Launch of Development Missile | |
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)for missile itself;12ft 2in(3.70m)for booster |
Diameter | 1.5 feet (0.47 m) |
Warhead | High explosive 150 pounds (68 kg) continuous rod, blast fragmentation or W60 low-yield nuclear warhead[1] |
Detonation mechanism | Proximity Fuse |
| |
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.[1] 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.
See also
References
- 1 2 Bendix SAM-N-8/RIM-50 Typhon LR Directory of U.S. Military Rockets and Missiles retrieved May 4, 2015
External links
- RIM-50 Typhon—GlobalSecurity.org
- Bendix SAM-N-8/RIM-50 Typhon LR—Directory of U.S. Military Rockets and Missiles
- Bendix SAM-N-9/RIM-55 Typhon MR—Directory of U.S. Military Rockets and Missiles
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