Draft:NK-9

Soviet rocket engine design From Wikipedia, the free encyclopedia

The NK-9 was a rocket engine designed and built in 1959 by the Kuznetsov Design Bureau. The NK designation was derived from the initials of chief designer Nikolay Kuznetsov. It was intended for the R-9 Desna, but lost this bid to the RD-111. It was then intended for the cruising stage of the Global Rocket 1, but that project was cancelled. The engine was developed into the NK-9V, with a higher expansion ratio, which was also cancelled. It was later developed into the NK-15 for the N1.[2]

  1. "NK-9". Encyclopedia Astronautica.
  2. website=%5b%5bEncyclopedia Astronautica%5d%5d "NK-9". {{cite web}}: Check |url= value (help); Missing pipe in: |url= (help)
Country of originSoviet Union
Date1959
Application1st/2nd-stage engine
Quick facts Country of origin, Date ...
NK-9
Country of originSoviet Union
Date1959
DesignerKuznetsov Design Bureau
Application1st/2nd-stage engine
SuccessorNK-15
Liquid-fuel engine
PropellantLOX / RG-1
CycleStaged combustion
PumpsTurbopump
Performance
Thrust, vacuum441 kN (99,000 lbf)
Thrust, sea-level360 kN (81,000 lbf)
Specific impulse, vacuum327 s (3.21 km/s)
Specific impulse, sea-level280 s (2.7 km/s)
References
References[1]
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