MAKS Tank

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Model: MAKS Tank. Gross Mass: 248,100 kg (546,900 lb). Empty Mass: 10,820 kg (23,850 lb). Thrust (vac): 0 N ( lbf). Isp: 437 sec. Burn time: 440 sec. Propellants: Lox/Kerosene/LH2. Isp(sl): 396 sec. Diameter: 6.38 m (20.93 ft). Span: 6.38 m (20.93 ft). Length: 32.10 m (105.30 ft). Country: Russia. No Engines: 1. Motor: None. Status: Development ended 1988. Cost $ : 5.000 million. First Flight: 1992. Used as: MAKS Orbiter. Used on Launch Vehicles: MAKS. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.