This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Application: Burlak stage 2. Used on stages: Burlak Stage 2. Used on launch vehicles: Burlak. Propellants: N2O4/UDMH Thrust(vac): 10,000 kgf. Thrust(vac): 98.00 kN. Isp: 330 sec. Isp (sea level): 230 sec. Burn time: 275 sec. Chambers: 1. Country: Russia. Status: Out of Production. Comments: Masses, thrust, specific impulse estimated based on total vehicle mass of 28.5 tonnes and first stage burn time of 140 seconds. Air launched from Tu-160 at 13,500 m, Mach 1.7 release conditions.
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Last update 12 March 2001.
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© Mark Wade, 2001 .