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MAKS Orbiter
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Gross Mass: 18,600 kg (41,000 lb). Empty Mass: 18,600 kg (41,000 lb). Thrust (vac): 3,618.771 kN (813,532 lbf). Isp: 437 sec. Burn time: 440 sec. Propellants: Lox/Kerosene/LH2. Isp(sl): 396 sec. Diameter: 3.00 m (9.80 ft). Span: 12.50 m (41.00 ft). Length: 19.30 m (63.30 ft). Country: Russia. No Engines: 1. Engine: RD-701. Status: Development ended 1988. Cost $ : 8.000 million. First Flight: 1992. Empty mass without 9300 kg payload.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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