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Titan LDC-2
Part of Titan LR91 stage series Family
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: 444.82 kN (99,999 lbf). Gross mass: 50,000 kg (110,000 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 316 s. Specific impulse sea level: 160 s. Burn time: 320 s. Height: 13.40 m (43.90 ft). Diameter: 4.57 m (14.99 ft). Span: 4.57 m (14.99 ft).

Cost $ : 4.640 million.



Country: USA. Engines: LR91-7. Launch Vehicles: Titan 3L2, Titan 3L4. Propellants: N2O4/Aerozine-50.

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