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
Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality

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Related Documents 2840-39-000-0732 2+ Documents (More...)
NOMIM 4080400216 MOTOR TURBOREACTOR PTR IAR-95 A continuous-combustion type power unit, may be with
RQST NE Updated Every Day 2840-39-000-0732 RQST Updated Every Day 2840-39-000-0732 RQST NE Related Documents
2840-39-000-0732 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0732
RQST NE Updated Every Day 2840-39-000-0732 RQST Updated Every Day 2840-39-000-0732 RQST NE Related Documents
2840-39-000-0732 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0732
2002 2840-39-000-0733 Turbo-Jet Engine MOTOR VIPER 633-47RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0732
Restrictions 2840-39-000-0732
End Users 2840-39-000-0732
- Romania (WR)
Approved Sources 2840-39-000-0732
- Part Number
- Manufacturer
- Status
- NOMIM 4080400216
- Manufacturer
- 0062L - Biroul National De Codificare (Active)
- Definitive Standard
- Definitive Standard
- MOTOR TURBOREACTOR PTR IAR-95
- 0062L - Biroul National De Codificare (Active)
- Secondary Buy
- Secondary Buy
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