2840-39-000-0726

Turbo-Jet Engine

2840390000726 390000726 NOMIM 4080400154 MOTOR R11F2S-300 (MIG-21RFM)

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

2840-39-000-0726 ENGINE,TURBO-JET 2840390000726 390000726

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
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2840-39-000-0726 Related Documents Related Documents 2840-39-000-0726 3+ Documents (More...)

NOMIM 4080400154 MOTOR R11F2S-300 (MIG-21RFM) A continuous-combustion type power unit, may be with or
RQST NE Updated Every Day 2840-39-000-0726 RQST Updated Every Day 2840-39-000-0726 RQST NE Related Documents
2840-39-000-0726 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0726
2840-39-000-0739 Turbo-Jet Engine MOTOR VIPER MK-623MRNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0726
Turbo-Jet Engine MOTOR R11F2S-300 (MIG-21RFM)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000
Engines, Aircraft, Prime Moving; and Components from Romania (RO) 000-0726 Turbo-Jet Engine MOTOR R11F2S-300 (MIG-21RFM

2840-39-000-0726 Demil Restrictions 2840-39-000-0726

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2840-39-000-0726 is a Turbo-Jet Engine

2840-39-000-0726 End Users End Users 2840-39-000-0726

Romania (WR)

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