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Liberty 1
LOx/Kerosene propellant rocket stage. .

Status: Development ended 1988. Thrust: 245.00 kN (55,078 lbf). Gross mass: 17,000 kg (37,000 lb). Unfuelled mass: 2,240 kg (4,930 lb). Specific impulse: 270 s. Specific impulse sea level: 230 s. Burn time: 157 s. Height: 10.20 m (33.40 ft). Diameter: 1.58 m (5.18 ft). Span: 1.58 m (5.18 ft).

Cost $ : 0.750 million.



Country: USA. Engines: Liberty-1. Launch Vehicles: Liberty. Propellants: Lox/Kerosene.

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