2840-14-384-8953
Turbine Engine Afterburner
2840143848953 143848953 502-563-812-0
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 2 Jun 1983
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-14-384-8953
Need Help?
Request a Quotation from participating marketplace vendors
Request a Quotation from participating marketplace vendors
Related Documents 2840-14-384-8953 1+ Documents (More...)
RQST NE Updated Every Day 2840-14-384-8953 RQST Updated Every Day 2840-14-384-8953 RQST NE Related Documents
2840-14-384-8953 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-384-8953
Turbine Engine Afterburner 2840143848953 502-563-812-0 A chamber in which additional fuel is injected
2840-14-384-8953 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-384-8953
Turbine Engine Afterburner 2840143848953 502-563-812-0 A chamber in which additional fuel is injected
Restrictions 2840-14-384-8953
End Users 2840-14-384-8953
- France (ZF)
Approved Sources 2840-14-384-8953
- Part Number
- Manufacturer
- Status
- 502-563-812-0
- Manufacturer
- F0301 - Safran Aircraft Engines (Active)
- Primary Buy
- Primary Buy
Similar Supply Items to 2840-14-384-8953
