Development of NK-8 engine, modified for supersonic operation.

Other design details:

Model NK-144 NK-144A

Tu-144 prototype


Year ? ?
Type bypass turbojet bypass turbojet
Full Afterburner
Thrust 17,500kg 18,150kg
Fuel consumption ?kg/kgf/hour ?kg/kgf/hour
Maximum without afterburner
Thrust 13,000kg 15,000kg
Fuel consumption ?kg/kgf/hour ?kg/kgf/hour
other parameters
Bypass ratio ?
Compression ?
Maximum turbine inlet temperature ?°K
Resource ?h
Length 5200mm
Maximum Diameter 1500mm
Weight ?kg
  • ...
  • NK-144, NK-22, NK-25
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