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Falcon 1-1
LOx/Kerosene propellant rocket stage. .

Status: Retired. Thrust: 369.00 kN (82,954 lbf). Gross mass: 22,993 kg (50,690 lb). Unfuelled mass: 1,505 kg (3,317 lb). Specific impulse: 300 s. Specific impulse sea level: 282 s. Burn time: 169 s. Height: 12.30 m (40.30 ft). Diameter: 1.70 m (5.50 ft).



Subtopics

Falcon 1e-1 LOx/Kerosene propellant rocket stage. .

Country: USA. Engines: Merlin 1A. Launch Vehicles: Falcon 1. Propellants: Lox/Kerosene. Agency: SpaceX.

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