2840-39-000-0729

Turbo-Jet Engine

2840390000729 390000729 NOMIM 4080400181 MOTOR TURBOREACTOR PTR IAR-99

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

2840-39-000-0729 ENGINE,TURBO-JET 2840390000729 390000729 1/1 — NSN 2840-39-000-0729 (Generic Image) 1/1

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2840-39-000-0729 Turbo-Jet Engine 2840390000729 390000729

NOMIM 4080400181 MOTOR TURBOREACTOR PTR IAR-99 A continuous-combustion type power unit, may be with
RQST NE Updated Every Day 2840-39-000-0729 RQST Updated Every Day 2840-39-000-0729 RQST NE Related Documents
2840-39-000-0729 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0729

https//www.nsnlookup.com
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Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO)

2002 2840-39-000-0724 Turbo-Jet Engine NOMIM 4080400136RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0729

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

2840-39-000-0728 Turbo-Jet Engine 2840390000728 390000728

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2002 2840-39-000-0729