2840-14-395-6735

Turbine Engine Afterburner

2840143956735 143956735 502-562-815-0

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

2840-14-395-6735 AFTERBURNER,TURBINE ENGINE 2840143956735 143956735

Managed by France
NSN Created on 30 Oct 1984
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-395-6735 AFTERBURNER,TURBINE ENGINE 2840143956735 143956735 1/1
NSN 2840-14-395-6735 (Generic Image) 1/1

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Turbine Engine Afterburner 2840143956735 502-562-815-0 A chamber in which additional fuel is injected

2840-14-395-6735 Demil Restrictions 2840-14-395-6735

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2840-14-395-6735 is a Turbine Engine Afterburner

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