2840-12-188-1516
Turbo-Jet Engine
2840121881516 121881516 RB199MK101R
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 2 Jan 1981
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-12-188-1516
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Related Documents 2840-12-188-1516 1+ Documents (More...)
Germany (DE) 4. 2840-12-188-1516 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 2840-12-188-1516 RQST Updated Every Day 2840-12-188-1516 RQST NE Related Documents
2840-12-188-1516 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-188-1516
RQST NE Updated Every Day 2840-12-188-1516 RQST Updated Every Day 2840-12-188-1516 RQST NE Related Documents
2840-12-188-1516 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-188-1516
Restrictions 2840-12-188-1516
End Users 2840-12-188-1516
- Germany (ZG)
- Italy (ZR)
Approved Sources 2840-12-188-1516
- Part Number
- Manufacturer
- Status
- RB199MK101R
- Manufacturer
- D3309 - Mtu Aero Engines Ag (Active)
- Primary Buy
- Primary Buy
- RB199MK101R
- A3460 - Ge Avio Srl (Active)
- Secondary Buy
- Secondary Buy
- RB199MK101R
- K0378 - Rolls-Royce Plc (Active)
- Secondary Buy
- Secondary Buy
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