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R-31 engine
Lyulka turbojet engine. MiG-25. Out of Production. Used in MiG-25. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.

AKA: R-31. Status: Out of Production. Number: 1 . Thrust: 91.20 kN (20,503 lbf). Specific impulse: 2,073 s. Burn time: 3,000 s.

Thrust (sl): 82.900 kN (18,637 lbf). Thrust (sl): 8,449 kgf.



Family: Turbojet. Country: Russia. Propellants: Air/Kerosene. Stages: MiG-25. Agency: Lyulka bureau. Bibliography: 303.

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