2840-12-700-5940

Turbine Engine Afterburner

2840127005940 127005940 VG95211-ML-127005940 RP260AL-000 RP-260AL 0501024033009

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 26 Sep 1992

Data Last Changed
January 2023

NATO Update Count
1

NATO Data Quality

2840-12-700-5940 AFTERBURNER,TURBINE ENGINE 2840127005940 127005940 1/1 — NSN 2840-12-700-5940 (Generic Image) 1/1

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2840-12-700-5940 Turbine Engine Afterburner 2840127005940

VG95211-ML-127005940 RP260AL-000 RP-260AL 0501024033009 A chamber in which additional fuel is injected
RQST NE Updated Every Day 2840-12-700-5940 RQST Updated Every Day 2840-12-700-5940 RQST NE Related Documents
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web browser . 1650-40-000-1194Aircraft Hydraulic-Pneumatic Servomechanism1650400001194 400001194 RP-260AL
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Turbine Engine Afterburner 2840127005940 2840-12-700-5940Turbine Engine Afterburner2840127005940

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Aircraft Hydraulic, Vacuum, and De-icing System Components from Slovakia (SK)

NSN Lookup of Items in Aircraft Hydraulic, Vacuum, and De-icing System Components managed by Slovakia (SK).