2840-14-517-9612
Turbine Engine Afterburner
2840145179612 145179612 307-075-360-0
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
Managed by France
NSN Created on 19 Jan 2000
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-14-517-9612
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Related Documents 2840-14-517-9612 1+ Documents (More...)
RQST NE Updated Every Day 2840-14-517-9612 RQST Updated Every Day 2840-14-517-9612 RQST NE Related Documents
2840-14-517-9612 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-517-9612
Turbine Engine Afterburner 2840145179612 307-075-360-0 A chamber in which additional fuel is injected
2840-14-517-9612 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-517-9612
Turbine Engine Afterburner 2840145179612 307-075-360-0 A chamber in which additional fuel is injected
Restrictions 2840-14-517-9612
End Users 2840-14-517-9612
- France (ZF)
Approved Sources 2840-14-517-9612
- Part Number
- Manufacturer
- Status
- 307-075-360-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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