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Kuznetsov NK-144


Kuznetsov NK-144


The Kuznetsov NK-144 is an afterburning turbofan engine made by the Soviet Kuznetsov Design Bureau. Used on the early models of the Tupolev Tu-144 supersonic aircraft, it was very inefficient and was replaced with the Kolesov RD-36-51 turbojet engine.

Specifications

Data from

General characteristics

  • Type: Twin-spool afterburning turbofan
  • Length:
  • Diameter:
  • Dry weight:

Components

  • Compressor: axial

Performance

  • Maximum thrust: 28,660 lbf (dry) 38,580 lbf (wet)
(127.40 kN 63,185 lbf to 171.2 kN
  • Overall pressure ratio: 14.2
  • Bypass ratio: 0.60
  • Air mass flow: 551 lb/s
  • Specific fuel consumption: 1.81 lb/lbf hour

References

External links

  • NK-144 on LeteckeMotory.cz (Czech)

Text submitted to CC-BY-SA license. Source: Kuznetsov NK-144 by Wikipedia (Historical)