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

2840-39-000-0729 ENGINE,TURBO-JET 2840390000729 390000729

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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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
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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
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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

2840-39-000-0729 Demil Restrictions 2840-39-000-0729

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

2840-39-000-0729 is a Turbo-Jet Engine

2840-39-000-0729 End Users End Users 2840-39-000-0729

Romania (WR)

2840-39-000-0729 Manufacturers Approved Sources 2840-39-000-0729

Part Number
Manufacturer
Status
NOMIM 4080400181
0062L - Biroul National De Codificare (Active)
Definitive Standard
RNCC 2 RNVC 2 DAC 4
MOTOR TURBOREACTOR PTR IAR-99
0062L - Biroul National De Codificare (Active)
Secondary Buy
RNCC 5 RNVC 2 DAC 4

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