2840-39-000-0732

Turbo-Jet Engine

2840390000732 390000732 NOMIM 4080400216 MOTOR TURBOREACTOR PTR IAR-95

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

2840-39-000-0732 ENGINE,TURBO-JET 2840390000732 390000732

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
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2840-39-000-0732 Turbo-Jet Engine 2840390000732 390000732
NOMIM 4080400216 MOTOR TURBOREACTOR PTR IAR-95 A continuous-combustion type power unit, may be with
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Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO)
2002 2840-39-000-0733 Turbo-Jet Engine MOTOR VIPER 633-47RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0732

2840-39-000-0732 Demil Restrictions 2840-39-000-0732

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-39-000-0732 is a Turbo-Jet Engine

2840-39-000-0732 End Users End Users 2840-39-000-0732

Romania (WR)

2840-39-000-0732 Manufacturers Approved Sources 2840-39-000-0732

Part Number
Manufacturer
Status
NOMIM 4080400216
0062L - Biroul National De Codificare (Active)
Definitive Standard
RNCC 2 RNVC 2 DAC 4
MOTOR TURBOREACTOR PTR IAR-95
0062L - Biroul National De Codificare (Active)
Secondary Buy
RNCC 5 RNVC 2 DAC 4

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