2840-21-850-2546
Turbo-Jet Engine
2840218502546 218502546 15700 89C10106-801
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 Canada
NSN Created on 6 Oct 1968
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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15700 89C10106-801 A continuous-combustion type power unit, may be with or without container, designed
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Restrictions 2840-21-850-2546
Approved Sources 2840-21-850-2546
- Part Number
- Manufacturer
- Status
- 15700
- Manufacturer
- 24235 - Williams International Co., L.L.C. (Active)
- Primary Buy
- Primary Buy
- 89C10106-801
- 88308 - Bombardier Inccanadair (Active)
- Secondary Buy
- Secondary Buy
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