2840-12-309-9724

Turbo-Jet Engine

2840123099724 123099724 RB199MK105-01

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

2840-12-309-9724 ENGINE,TURBO-JET 2840123099724 123099724

Managed by Germany
NSN Created on 24 Mar 1987
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-309-9724 ENGINE,TURBO-JET 2840123099724 123099724 1/1
NSN 2840-12-309-9724 (Generic Image) 1/1

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2840-12-309-9724 Turbo-Jet Engine 2840123099724 123099724
RB199MK105-01 A continuous-combustion type power unit, may be with or without container, designed to
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2840-12-309-9724 Demil Restrictions 2840-12-309-9724

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2840-12-309-9724 is a Turbo-Jet Engine

2840-12-309-9724 End Users End Users 2840-12-309-9724

Italy (ZR)

2840-12-309-9724 Manufacturers Approved Sources 2840-12-309-9724

Part Number
Manufacturer
Status
RB199MK105-01
D3309 - Mtu Aero Engines Ag (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 5
RB199MK105-01
U0702 - Turbo-Union Ltd (Replaced)
Secondary Buy
RNCC 5 RNVC 2 DAC 5

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