2840-39-000-0750
Turbo-Jet Engine
2840390000750 390000750 NOMIM 4080401016 MOTOR VK-1F
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
Marketplace 2840-39-000-0750
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Related Documents 2840-39-000-0750 5+ Documents (More...)
NOMIM 4080401016 MOTOR VK-1F A continuous-combustion type power unit, may be with or without container
RQST NE Updated Every Day 2840-39-000-0750 RQST Updated Every Day 2840-39-000-0750 RQST NE Related Documents
2840-39-000-0750 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0750
RQST NE Updated Every Day 2840-39-000-0750 RQST Updated Every Day 2840-39-000-0750 RQST NE Related Documents
2840-39-000-0750 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0750
Turbo-Jet Engine 2840390000750 390000750 -14-538-6282 Turbo-Jet Engine 2840145386282 145386282
Turbo-Jet Engine 2840390000750 390000750 Day 2840-39-000-0750 RQST NE Related Documents https//
538-6282 Turbo-Jet Engine 2840145386282145386282 325-6740 Turbo-Jet Engine 2840143256740 143256740 390000750
Turbo-Jet Engine 2840390000750 390000750 Day 2840-39-000-0750 RQST NE Related Documents https//
538-6282 Turbo-Jet Engine 2840145386282145386282 325-6740 Turbo-Jet Engine 2840143256740 143256740 390000750
Turbo-Jet Engine 2840390000750 390000750 Turbo-Jet Engine 2840993047082 993047082 522-6505 2840
www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5169 Turbo-Jet Engine 2840145105169145105169 2840390000750
-6282 Turbo-Jet Engine 2840145386282 145386282 325-6740 Turbo-Jet Engine 2840143256740 143256740 390000750
www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5169 Turbo-Jet Engine 2840145105169145105169 2840390000750
-6282 Turbo-Jet Engine 2840145386282 145386282 325-6740 Turbo-Jet Engine 2840143256740 143256740 390000750
CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0750
Turbo-Jet Engine 2840390000750 390000750 -14-538-6282 Turbo-Jet Engine 2840145386282 145386282
/www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-325-6740 Turbo-Jet Engine 2840143256740143256740 390000750
Turbo-Jet Engine 2840390000750 390000750 -14-538-6282 Turbo-Jet Engine 2840145386282 145386282
/www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-325-6740 Turbo-Jet Engine 2840143256740143256740 390000750
Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) Feb 2002 2840-39-000-0750
522-6505 2840-14-510-5169 2840-14-323-7565 2840-39-000-0731 2840-14-538-6282 2840-14-325-6740 2840-39-000-0750
522-6505 2840-14-510-5169 2840-14-323-7565 2840-39-000-0731 2840-14-538-6282 2840-14-325-6740 2840-39-000-0750
Restrictions 2840-39-000-0750
End Users 2840-39-000-0750
- Romania (WR)
Approved Sources 2840-39-000-0750
- Part Number
- Manufacturer
- Status
- NOMIM 4080401016
- Manufacturer
- 0062L - Biroul National De Codificare (Active)
- Definitive Standard
- Definitive Standard
- MOTOR VK-1F
- 0062L - Biroul National De Codificare (Active)
- Secondary Buy
- Secondary Buy
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