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RD-36-41
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Manufacturer Name: RD-36-41. Designer: Lyulka. Application: T-4. Propellants: Air/Kerosene. Thrust(vac): 158.400 kN (35,610 lbf). Thrust(sl): 144.000 kN (32,372 lbf). Isp: 1,980 sec. Burn time: 5,400 sec. Chambers: 1. Country: Russia. Status: Out of Production. Used in Sukhoi March 3 aircraft. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.
RD-36-41 used on Rocket Stages
Bibliography and Further Reading - Gunston, Bill, The Osprey Encylopedia of Russian Aircraft 1975-1995, Osprey, London, 1995. ISBN: 1855324059. The greatest single reference on Soviet winged aircraft. More at amazon.com...
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