Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
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.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use