2840-14-382-4172

Turbine Engine Afterburner

2840143824172 143824172 057-01-012

A chamber in which additional fuel is injected into, the exhaust gases, and reheating the gases to develop increased thrust. It consists of combustion area, flame holders, injection nozzles and an exhaust ejector. View more Turbine Engine Afterburner

2840-14-382-4172 AFTERBURNER,TURBINE ENGINE 2840143824172 143824172

Managed by France
NSN Created on 17 Feb 1983
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-382-4172 AFTERBURNER,TURBINE ENGINE 2840143824172 143824172 1/1
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2840-14-382-4172 Related Documents Related Documents 2840-14-382-4172 3+ Documents (More...)

Documents 2840-14-524-2477 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-382-4172
Turbine Engine Afterburner 2840143824172 2840-14-382-4172 2840143824172 143824172 is a chamber
2840-14-365-3567 Turbine Engine Afterburner 303-052-805-0RNCC: 3 | RNVC: 2 | DAC: 2 19 Sep 1980 2840-14-382-4172
Gas Turbine Engine Combustion Chamber Liner 047-01-114RNCC: 3 | RNVC: 2 | DAC: 5 7 Mar 2001 2840-14-382-4172

2840-14-382-4172 Demil Restrictions 2840-14-382-4172

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

2840-14-382-4172 is a Turbine Engine Afterburner

2840-14-382-4172 End Users End Users 2840-14-382-4172

Spain (YB)
France (ZF)

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