2840-12-700-5943

Turbine Engine Afterburner

2840127005943 127005943 VG95211-ML-127005943 RP280-000 RP-280 0501024040989

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

2840-12-700-5943 AFTERBURNER,TURBINE ENGINE 2840127005943 127005943

Managed by Germany
NSN Created on 26 Sep 1992
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-12-700-5943 AFTERBURNER,TURBINE ENGINE 2840127005943 127005943 1/1
NSN 2840-12-700-5943 (Generic Image) 1/1

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VG95211-ML-127005943 RP280-000 RP-280 0501024040989 A chamber in which additional fuel is injected into
2840-12-700-5943 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-700-5943
2840-12-700-5943 RQST NE Restrictions Restrictions 2840-12-700-5943 DEMIL: | DEMILI : | CRITICALITY :
web browser . 1650-40-000-1193Aircraft Hydraulic-Pneumatic Servomechanism1650400001193 400001193 RP-280
Documents 1650-40-000-1193 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/de 2840-12-700-5943
Turbine Engine Afterburner 2840127005943 2840-12-700-5943Turbine Engine Afterburner2840127005943

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