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Riksha
Russian orbital launch vehicle. New design launch vehicle based on SLBM technology.

Status: Design 1994. Payload: 1,700 kg (3,700 lb). Apogee: 200 km (120 mi).

LEO Payload: 1,700 kg (3,700 lb) to a 200 km orbit. Payload: 1,160 kg (2,550 lb) to a 1000 km orbit.



Family: orbital launch vehicle. Country: Russia. Engines: RD-182, RD-169, RD-185, RD-190, RD-183, RD-184. Agency: Makeyev bureau. Bibliography: 193.

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