MIGAKS

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MIGAKS

Part of VVS 1993

Russian winged orbital launch vehicle. Turbojet/ramjet-powered two stage to orbit horizontal takeoff / horizontal landing vehicle. Mach 6 stage separation. The orbiter had a 2000 km cross-range capability with landing on airfields with runways of 3500 m length or more.

Status: Study 1993. Payload: 12,600 kg (27,700 lb). Gross mass: 420,000 kg (920,000 lb). Apogee: 200 km (120 mi).

LEO Payload: 12,600 kg (27,700 lb) to a 200 km orbit at 51.00 degrees.

Family: orbital launch vehicle, Winged. Country: Russia. Agency: MiG.

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