Falcon 1e (original) (raw)

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Part of Falcon

Version of Falcon 1 with stretched first stage and much more powerful Merlin engine.

Status: Retired. Payload: 1,010 kg (2,220 lb). Thrust: 556.00 kN (124,993 lbf). Gross mass: 46,760 kg (103,080 lb). Height: 27.40 m (89.80 ft). Diameter: 1.70 m (5.50 ft). Span: 1.70 m (5.50 ft). Apogee: 200 km (120 mi).

LEO Payload: 1,010 kg (2,220 lb) to a 200 km orbit at 9.10 degrees. Payload: 560 kg (1,230 lb) to a 700 km SSO. Launch Price $: 9.100 million in 2008 dollars. Boost Propulsion: Lox-Kerosene. Cruise Thrust: 33.300 kN (7,486 lbf). Cruise Thrust: 3,400 kgf. Cruise engine: Kestrel. Initial Operational Capability: 2010.

More at: Falcon 1e.

Family: LCLVs, low cost, orbital launch vehicle. Country: USA. Stages: Falcon 1-2, Falcon 1e-1. Agency: SpaceX.

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