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Venturestar
Part of X-33
American SSTO winged orbital launch vehicle. Production reusable single-stage-to-orbit launch vehicle using technology developed in X-33 test bed.

Status: Cancelled 1999. Payload: 26,800 kg (59,000 lb). Thrust: 13,390.00 kN (3,010,190 lbf). Gross mass: 991,000 kg (2,184,000 lb). Height: 39.70 m (130.20 ft). Diameter: 39.00 m (127.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 26,800 kg (59,000 lb) to a 185 km orbit at 28.00 degrees.

Family: orbital launch vehicle, Spaceplane, SSTO, US Rocketplanes, Winged. Country: USA. Engines: RS-2200. Launch Vehicles: Venturestar. Propellants: Lox/LH2. Agency: Lockheed.
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