Zenit-2

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Model: Zenit-2. Gross Mass: 90,600 kg (199,700 lb). Empty Mass: 9,000 kg (19,800 lb). Thrust (vac): 912.000 kN (205,025 lbf). Isp: 349 sec. Burn time: 315 sec. Propellants: Lox/Kerosene. Isp(sl): 0 sec. Diameter: 3.90 m (12.70 ft). Span: 3.90 m (12.70 ft). Length: 11.50 m (37.70 ft). Country: Ukraine. No Engines: 1. Motor: RD-120. Status: Active. Cost $ : 15.000 million. First Flight: 1976. Last Flight: 2008. No Launched: 85. No Failed: 5. Used on Launch Vehicles: Zenit. 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.