Titan LDC-1

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Titan LDC-1

Part of Titan LR87 stage series

N2O4/Aerozine-50 propellant rocket stage. 15 foot diameter core Titan proposed in 1960's for space station logistics. Masses estimated.

Status: Study 1965. Thrust: 4,344.46 kN (976,674 lbf). Gross mass: 350,000 kg (770,000 lb). Unfuelled mass: 20,000 kg (44,000 lb). Specific impulse: 296 s. Specific impulse sea level: 258 s. Burn time: 210 s. Height: 29.90 m (98.00 ft). Diameter: 4.57 m (14.99 ft). Span: 4.57 m (14.99 ft).

Cost $ : 11.600 million. No Engines: 4.

Country: USA. Engines: LR87-7. Launch Vehicles: Titan 3L2, Titan 3L4. Propellants: N2O4/Aerozine-50.

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