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Weapons of Mass Destruction (WMD)




Trident I C-4 FBM / SLBM

Specifications

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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