2840-12-041-9845
Turbo-Jet Engine
2840120419845 120419845
Cancelled - Replaced by NSN 2840-14-241-9175
A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust. View more Turbo-Jet Engine
Managed by Germany
Data Last Changed
January 2024
January 2024
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-12-041-9845
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2840-12-095-1694 Fluid Pressure Line Multiple Connector
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