| 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) |
| 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 |
|
|
|
| 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.