2840-39-000-0725

Turbo-Jet Engine

2840390000725 390000725 NOMIM 4080400145 MOTOR R11F2SSK-300(MIG-21M,RFMM)

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

2840-39-000-0725 ENGINE,TURBO-JET 2840390000725 390000725

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
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2840-39-000-0725 Related Documents Related Documents 2840-39-000-0725 3+ Documents (More...)

NOMIM 4080400145 MOTOR R11F2SSK-300(MIG-21M,RFMM) A continuous-combustion type power unit, may be with
RQST NE Updated Every Day 2840-39-000-0725 RQST Updated Every Day 2840-39-000-0725 RQST NE Related Documents
2840-39-000-0725 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0725
An item consisting of a refrigeration compressor https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0725
Turbo-Jet Engine 2840390000725 390000725 2840-39-000-0725Turbo-Jet Engine2840390000725 390000725
NOMIM 4080400145 MOTOR R11F2SSK-300(MIG-21M,RFMM) A 2840-39-000-0725 Turbo-Jet Engine 2840390000725390000725
Feb 2002 2840-39-000-0735 Turbo-Jet Engine MOTOR D-30-KURNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0725
Turbo-Jet Engine MOTOR R11F2SSK-300(MIG-21M,RFMM)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39

2840-39-000-0725 Demil Restrictions 2840-39-000-0725

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2840-39-000-0725 is a Turbo-Jet Engine

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