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Model: SpaceShipOne. Gross Mass: 3,600 kg (7,900 lb). Empty Mass: 1,200 kg (2,600 lb). Thrust (vac): 73.500 kN (16,523 lbf). Isp: 250 sec. Burn time: 80 sec. Propellants: N2O/Solid. Propellant Formulation: N2O/HTPB. Diameter: 1.52 m (4.98 ft). Span: 5.00 m (16.40 ft). Country: USA. No Engines: 1. Motor: SpaceDev Hybrid. Status: Retired 2004. First Flight: 2002. Last Flight: 2004. No Launched: 56. Wing area 15 sq m. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |