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Titan 1-1
Part of Titan LR87 stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Study 1959. Thrust: 1,467.91 kN (329,999 lbf). Gross mass: 76,203 kg (167,998 lb). Unfuelled mass: 4,000 kg (8,800 lb). Specific impulse: 290 s. Specific impulse sea level: 256 s. Burn time: 138 s. Height: 16.00 m (52.00 ft). Diameter: 3.05 m (10.00 ft). Span: 3.05 m (10.00 ft).

Cost $ : 10.000 million. No Engines: 2.



Country: USA. Engines: LR87-3. Launch Vehicles: Titan I, Super-Jupiter, Juno V-A, Juno V-B, Saturn A-1. Propellants: Lox/Kerosene.

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