This page no longer updated from 31 October 2001. Latest version can be found at RD-36-41

Manufacturer Name: RD-36-41. Designer: Lyulka. Application: T-4. Used on stages: T-4. Propellants: Air/Kerosene Thrust(vac): 16,150 kgf. Thrust(vac): 158.40 kN. Isp: 1,980 sec. Burn time: 5,400 sec. Chambers: 1. Country: Russia. Status: Out of Production. References: 303 . Comments: Used in Sukhoi March 3 aircraft. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.
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Last update 12 March 2001.
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© Mark Wade, 2001 .