2840-12-165-3532
Turbine Engine Afterburner
2840121653532 121653532 VG95211-ML-121653532 7013M40G03
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 Germany
NSN Created on 23 Apr 1976
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-12-165-3532
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Related Documents 2840-12-165-3532 1+ Documents (More...)
VG95211-ML-121653532 7013M40G03 A chamber in which additional fuel is injected into, the exhaust gases
RQST NE Updated Every Day 2840-12-165-3532 RQST Updated Every Day 2840-12-165-3532 RQST NE Related Documents
2840-12-165-3532 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-165-3532
RQST NE Updated Every Day 2840-12-165-3532 RQST Updated Every Day 2840-12-165-3532 RQST NE Related Documents
2840-12-165-3532 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-165-3532
Restrictions 2840-12-165-3532
End Users 2840-12-165-3532
- Germany (ZG)
- Greece (ZU)
Approved Sources 2840-12-165-3532
- Part Number
- Manufacturer
- Status
- VG95211-ML-121653532
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- 7013M40G03
- D3309 - Mtu Aero Engines Ag (Active)
- Primary Buy
- Primary Buy
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