Falcon 1e-1 (original) (raw)

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Falcon 1e-1

Part of Falcon 1-1

LOx/Kerosene propellant rocket stage. .

Status: Retired. Thrust: 615.50 kN (138,370 lbf). Gross mass: 42,168 kg (92,964 lb). Unfuelled mass: 2,712 kg (5,978 lb). Specific impulse: 304 s. Specific impulse sea level: 275 s. Burn time: 169 s. Height: 18.60 m (61.00 ft). Diameter: 1.70 m (5.50 ft).

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

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