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Winged orbital launch vehicle. Year: 2006. Family: Winged. Country: USA. Status: Development ended 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).
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