2840-12-309-9727
Turbo-Jet Engine
2840123099727 123099727 RB199MK105
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 24 Mar 1987
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-12-309-9727
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Restrictions 2840-12-309-9727
End Users 2840-12-309-9727
- Germany (ZG)
Approved Sources 2840-12-309-9727
- Part Number
- Manufacturer
- Status
- RB199MK105
- Manufacturer
- D3309 - Mtu Aero Engines Ag (Active)
- Primary Buy
- Primary Buy
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