2840-14-516-2450
Turbine Engine Afterburner
2840145162450 145162450 307-075-361-0
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 15 Sep 1999
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-14-516-2450
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RQST NE Updated Every Day 2840-14-516-2450 RQST Updated Every Day 2840-14-516-2450 RQST NE Related Documents
2840-14-516-2450 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-516-2450
Turbine Engine Afterburner 2840145162450 307-075-361-0 A chamber in which additional fuel is injected
2840-14-516-2450 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-516-2450
Turbine Engine Afterburner 2840145162450 307-075-361-0 A chamber in which additional fuel is injected
Restrictions 2840-14-516-2450
End Users 2840-14-516-2450
- France (ZF)
Approved Sources 2840-14-516-2450
- Part Number
- Manufacturer
- Status
- 307-075-361-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
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