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
NATO Data Quality
2840-39-000-0725 ENGINE,TURBO-JET 2840390000725 390000725 1/1
NSN 2840-39-000-0725 (Generic Image) 1/1

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2840-39-000-0725 Related Documents Related Documents 2840-39-000-0725 2+ Documents (More...)

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
Jan 2000 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

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

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

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