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Winged orbital launch vehicle. Family: Sled-Launched. 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.

Manufacturer: MiG. LEO Payload: 9,000 kg (19,800 lb). to: 200 km Orbit. at: 51.00 degrees. Total Mass: 300,000 kg (660,000 lb). Core Diameter: 19.70 m (64.60 ft). Total Length: 54.10 m (177.40 ft).


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