This page no longer updated from 31 October 2001. Latest version can be found at MiG-2000

Family: Winged. Country: Russia. Status: Study 1993.

Sled-launched single stage to orbit vehicle with air-breathing propulsion to Mach 5 (subsonic combustion). The sled would accelerate the launch vehicle to Mach 0.8. Propellants wer slush hydrogen and liquid oxygen. The vehicle would have a 3000 km cross-range on re-entry.


LEO Payload: 9,000 kg. to: 200 km Orbit. at: 51.0 degrees. Total Mass: 300,000 kg. Core Diameter: 19.7 m. Total Length: 54.1 m.

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