Trident I C-4 FBM / SLBM
Specifications |
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| Designation: | UGM-96A Trident I C4 |
| Primary Function: | Strategic Nuclear Deterrence |
| Contractor: | Lockheed Martin Missiles & Space, USA |
| Propulsion: | Three-stage solid-propellant rocket |
| Length: | 34ft (10.2m) |
| Diameter: | 6ft 2in (1.9m) |
| Launch Weight: | 73,000lbs (32,850kg) |
| Range: | 4,350nm (5,000mi; 8,050km) |
| Max. Altitude: | Sub-orbital |
| Guidance: | Inertial |
| Warheads: | 8 100-KT W76 warheads in 8 Mk4 MIRVs |
| Deployed: | 1979 |
| Unit Cost: | $13 Million US [1979] |
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