2840-12-198-1609
Turbo-Jet Engine
2840121981609 121981609 RB199MK103
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 27 Dec 1983
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-12-198-1609
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Related Documents 2840-12-198-1609 3+ Documents (More...)
RB199MK103 A continuous-combustion type power unit, may be with or without container, designed to exert
Germany (DE) 4. 2840-12-198-1609 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 2840-12-198-1609 RQST Updated Every Day 2840-12-198-1609 RQST NE Related Documents
Germany (DE) 4. 2840-12-198-1609 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 2840-12-198-1609 RQST Updated Every Day 2840-12-198-1609 RQST NE Related Documents
JavaScript in your web browser . 2840-99-766-0508Turbo-Jet Engine2840997660508 997660508 JJ111177 RB199MK103
Turbo-Jet Engine 2840121981609 121981609 RB199MK103 2 JJ111177 K0378 - Rolls-Royce Plc (Active)
2 JJ111177 K0378 - Rolls-Royce Plc (Active) Incomplete Secondary Reference RNCC 5 RNVC 1 DAC 2 RB199MK103
Turbo-Jet Engine 2840121981609 121981609 RB199MK103 2 JJ111177 K0378 - Rolls-Royce Plc (Active)
2 JJ111177 K0378 - Rolls-Royce Plc (Active) Incomplete Secondary Reference RNCC 5 RNVC 1 DAC 2 RB199MK103
JavaScript in your web browser . 2840-99-766-0507Turbo-Jet Engine2840997660507 997660507 JJ111177 RB199MK103
Turbo-Jet Engine 2840121981609 121981609 Turbo-Jet Engine 2840997660507997660507 JavaScript in
your web browser . 2840-99-766-0507Turbo-Jet Engine2840997660507 997660507JJ111177 RB199MK103 2 JJ111177
Turbo-Jet Engine 2840121981609 121981609 Turbo-Jet Engine 2840997660507997660507 JavaScript in
your web browser . 2840-99-766-0507Turbo-Jet Engine2840997660507 997660507JJ111177 RB199MK103 2 JJ111177
Restrictions 2840-12-198-1609
End Users 2840-12-198-1609
- Germany (ZG)
- United Kingdom (ZK)
- Italy (ZR)
Approved Sources 2840-12-198-1609
- Part Number
- Manufacturer
- Status
- RB199MK103
- Manufacturer
- D3309 - Mtu Aero Engines Ag (Active)
- Primary Buy
- Primary Buy
- RB199MK103
- A3460 - Ge Avio Srl (Active)
- Secondary Buy
- Secondary Buy
- RB199MK103
- K0378 - Rolls-Royce Plc (Active)
- Secondary Buy
- Secondary Buy
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