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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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