This page no longer updated from 31 October 2001. Latest version can be found at Venturestar

Family: Winged. Country: USA. Status: Development.

Production reusable single-stage-to-orbit launch vehicle using technology developed in X-33 testbed.


LEO Payload: 26,800 kg. to: 185 km Orbit. at: 28.0 degrees. Liftoff Thrust: 1,365,000 kgf. Total Mass: 991,000 kg. Core Diameter: 39.0 m. Total Length: 39.7 m.

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Last update 12 March 2001.
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© Mark Wade, 2001 .