2840-99-766-0508

Turbo-Jet Engine

2840997660508 997660508 JJ111177 RB199MK103-02

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

2840-99-766-0508 ENGINE,TURBO-JET 2840997660508 997660508

Managed by United Kingdom
NSN Created on 2 Sep 1989
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-99-766-0508 ENGINE,TURBO-JET 2840997660508 997660508 1/1
NSN 2840-99-766-0508 (Generic Image) 1/1

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JJ111177 RB199MK103-02 A continuous-combustion type power unit, may be with or without container, designed
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Engine2840997660508 997660508 JJ111177 RB199MK103 Turbo-Jet Engine 2840121981609121981609RB199MK103
2 JJ111177 K0378 - Rolls-Royce Plc (Active) 2 JJ111177 K0378 - Rolls-Royce Plc (Active) Incomplete Secondary
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Engine2840997660508 997660508 JJ111177 NumberManufacturerStatusRB199MK103-02 K0378 - Rolls-Royce Plc

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