2840-14-322-2301

Turbine Engine Afterburner

2840143222301 143222301 502-563-800-0

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

2840-14-322-2301 AFTERBURNER,TURBINE ENGINE 2840143222301 143222301

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-322-2301 AFTERBURNER,TURBINE ENGINE 2840143222301 143222301 1/1
NSN 2840-14-322-2301 (Generic Image) 1/1

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Turbine Engine Afterburner 2840143222301 502-563-800-0 A chamber in which additional fuel is injected

2840-14-322-2301 Demil Restrictions 2840-14-322-2301

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2840-14-322-2301 is a Turbine Engine Afterburner

2840-14-322-2301 End Users End Users 2840-14-322-2301

Spain (YB)
Kuwait (YK)
France (ZF)

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