2840-39-000-0721

Turbo-Jet Engine

2840390000721 390000721 NOMIM 4080300116 MOTOR R27F2M-300

A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust. View more Turbo-Jet Engine

Managed by Romania

NSN Created on 25 Feb 2002

Data Last Changed
July 2023

NATO Update Count
1

NATO Data Quality

2840-39-000-0721 ENGINE,TURBO-JET 2840390000721 390000721 1/1 — NSN 2840-39-000-0721 (Generic Image) 1/1

Marketplace 2840-39-000-0721

Need Help?
Request a Quotation from participating marketplace vendors

Updated Every Day

2840-39-000-0721 RQST NE

Updated Every Day

2840-39-000-0721 RQST

Updated Every Day

2840-39-000-0721 RQST NE

Related Documents 2840-39-000-0721 3+ Documents (More...)

https//www.nsnlookup.com
/fsg-28/fsc-2840/ro

2840-39-000-0721 Turbo-Jet Engine 2840390000721 390000721

NOMIM 4080300116 MOTOR R27F2M-300 A continuous-combustion type power unit, may be with or without container
RQST NE Updated Every Day 2840-39-000-0721 RQST Updated Every Day 2840-39-000-0721 RQST NE Related Documents
2840-39-000-0721 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0721

https//www.nsnlookup.com
/fsg-28/fsc-2840

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO)

Mar 2002 2840-39-000-0924 Turbo-Jet Engine MOTOR RD-45FARNCC: 5 | RNVC: 2 | DAC: 4 7 Mar 2002 2840-39-000-0721

https//www.nsnlookup.com
/fsg-28/fsc-2840/ro

2840-39-000-0739 Turbo-Jet Engine 2840390000739 390000739

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2002 2840-39-000-0721