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RD-56M
Part of RD-56 Family
Isayev LOx/LH2 rocket engine. Originally developed for Proton and Angara upper stage KVRB with planned first flight 1995. Finally flown on 12KRB upper stage for India's GSLV. First flight 2001.

AKA: 11D56M;KVD-1M. Status: In development. Date: 1994-. Number: 4 . Thrust: 73.58 kN (16,541 lbf). Specific impulse: 461 s.



Country: Russia. Spacecraft: KVRB. Launch Vehicles: N1F Sr, GSLV. Propellants: Lox/LH2. Stages: N1 Block Sr, Proton KM-4, Angara KVRB, GSLV-3 stage. Agency: Isayev bureau.

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