2840-14-385-3830

Turbine Engine Afterburner

2840143853830 143853830 0308327310

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

2840-14-385-3830 AFTERBURNER,TURBINE ENGINE 2840143853830 143853830

Managed by France
NSN Created on 26 Jul 1983
Data Last Changed
January 2023
NATO Update Count
1
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2840-14-385-3830 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-385-3830
Turbine Engine Afterburner 2840143853830 0308327310 A chamber in which additional fuel is injected into
RQST NE Updated Every Day 2840-14-385-3830 RQST Updated Every Day 2840-14-385-3830 RQST NE Restrictions
CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-385-3830
Turbine Engine Afterburner 2840143853830 Every Day 2840-14-385-3830 RQST NE Restrictions https/
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Turbine Engine Afterburner 2840142920486 253-4693 2840-12-700-5941 2840-14-299-6117 -2840/fr 2840-14-385-3830
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2840-12-700-5941 2840-14-299-6117 2840-14-314-6042 2840-14-353-6932 2840-14-330-4296 Afterburner 2840143853830

2840-14-385-3830 Demil Restrictions 2840-14-385-3830

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2840-14-385-3830 is a Turbine Engine Afterburner

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