2840-14-305-4390

Turbine Engine Afterburner

2840143054390 143054390 502-557-901-0

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

2840-14-305-4390 AFTERBURNER,TURBINE ENGINE 2840143054390 143054390

Managed by France
NSN Created on 1 Jan 1974
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-305-4390 AFTERBURNER,TURBINE ENGINE 2840143054390 143054390 1/1
NSN 2840-14-305-4390 (Generic Image) 1/1

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Turbine Engine Afterburner 2840143054390 502-557-901-0 A chamber in which additional fuel is injected

2840-14-305-4390 Demil Restrictions 2840-14-305-4390

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2840-14-305-4390 is a Turbine Engine Afterburner

2840-14-305-4390 End Users End Users 2840-14-305-4390

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