2840-12-359-6095
Turbo-Jet Engine
2840123596095 123596095 EJ200-101
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
NSN Created on 20 Feb 2003
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
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Marketplace 2840-12-359-6095
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Related Documents 2840-12-359-6095 5+ Documents (More...)
Documents 2840-99-766-0507 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-359-6095
Turbo-Jet Engine 2840123596095 123596095 https//www.nsnlookup.com /nato/nato-stock-numbers/inc
Turbo-Jet Engine 2840123596095 123596095 https//www.nsnlookup.com /nato/nato-stock-numbers/inc
https//www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet Engine (INC 02007) 2 Sep 1989 2840-12-359-6095
2 19 Jun 1999 4930-99-950-2925 Lubricator NN 13971 G01RNCC: 5 | RNVC: 2 | DAC: 2 16 Sep 1999 2840-12-359-6095
Apr 1991 2840-99-766-0507 Turbo-Jet Engine RB199MK103-01RNCC: 5 | RNVC: 2 | DAC: 2 2 Sep 1989 2840-12-359-6095
2840-12-371-9310 2840123719310 123719310 is 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.
Restrictions 2840-12-359-6095
End Users 2840-12-359-6095
- Germany (ZG)
- United Kingdom (ZK)
- Italy (ZR)
Approved Sources 2840-12-359-6095
- Part Number
- Manufacturer
- Status
- EJ200-101
- Manufacturer
- C7471 - Eurojet Turbo Gmbh (Active)
- Primary Buy
- Primary Buy
- EJ200-101
- K0378 - Rolls-Royce Military Aero Engines (Active)
- Secondary Buy
- Secondary Buy
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