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NK-231
Kuznetsov turbofan engine. Tu-160. Development ended 1992. Turbofan engine used in Tu-160. Thrust is maximum sea level thrust; specific impulse is sea level value at that thrust.

Status: Development ended 1992. Thrust: 226.50 kN (50,919 lbf). Specific impulse: 1,980 s. Burn time: 58,000 s.

Thrust (sl): 205.900 kN (46,288 lbf). Thrust (sl): 21,000 kgf.

Family: Turbofan. Country: Russia. Launch Vehicles: Burlak. Propellants: Air/Kerosene. Stages: Tu-160. Agency: Kuznetsov bureau. Bibliography: 303.
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