| Venturestar |
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Winged orbital launch vehicle. Family: VTOVL. Country: USA. Status: Cancelled 1999. Production reusable single-stage-to-orbit launch vehicle using technology developed in X-33 testbed.
Manufacturer: Lockheed. LEO Payload: 26,800 kg (59,000 lb). to: 185 km Orbit. at: 28.00 degrees. Associated Spacecraft: Venturestar. Liftoff Thrust: 13,390.000 kN (3,010,190 lbf). Total Mass: 991,000 kg (2,184,000 lb). Core Diameter: 39.00 m (127.00 ft). Total Length: 39.70 m (130.20 ft). 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. |