2840-39-000-0923
Turbo-Jet Engine
2840390000923 390000923 NOMIM 4080401025 MOTOR VK-1A (HONG-5)
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 7 Mar 2002
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-39-000-0923
Need Help?
Request a Quotation from participating marketplace vendors
Request a Quotation from participating marketplace vendors
Related Documents 2840-39-000-0923 4+ Documents (More...)
NOMIM 4080401025 MOTOR VK-1A (HONG-5) A continuous-combustion type power unit, may be with or without
RQST NE Updated Every Day 2840-39-000-0923 RQST Updated Every Day 2840-39-000-0923 RQST NE Related Documents
2840-39-000-0923 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0923
RQST NE Updated Every Day 2840-39-000-0923 RQST Updated Every Day 2840-39-000-0923 RQST NE Related Documents
2840-39-000-0923 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0923
from Belgium (BE) 22 Apr 1976 7125-13-116-8174 https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0923
Turbo-Jet Engine 2840390000923 390000923 your web browser . 2840-39-000-0923Turbo-Jet Engine2840390000923
390000923 NOMIM 4080401025 MOTOR VK-1A /fsg-28/fsc-2840/ro 2840-39-000-0923 Turbo-Jet Engine 2840390000923390000923
Turbo-Jet Engine 2840390000923 390000923 your web browser . 2840-39-000-0923Turbo-Jet Engine2840390000923
390000923 NOMIM 4080401025 MOTOR VK-1A /fsg-28/fsc-2840/ro 2840-39-000-0923 Turbo-Jet Engine 2840390000923390000923
Feb 2002 2840-39-000-0741 Turbo-Jet Engine MOTOR VIPERRNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0923
Turbo-Jet Engine MOTOR VK-1A (HONG-5)RNCC: 5 | RNVC: 2 | DAC: 4 7 Mar 2002 2840-39-000-0742 Turbo-Jet
Turbo-Jet Engine MOTOR VK-1A (HONG-5)RNCC: 5 | RNVC: 2 | DAC: 4 7 Mar 2002 2840-39-000-0742 Turbo-Jet
-2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2840-39-000-0923
Turbo-Jet Engine MOTOR VK-1A (HONG-5)RNCC: 5 | RNVC: 2 | DAC: 4 7 Mar 2002 2840-39-000-0742 Restrictions
Turbo-Jet Engine MOTOR VK-1A (HONG-5)RNCC: 5 | RNVC: 2 | DAC: 4 7 Mar 2002 2840-39-000-0742 Restrictions
Restrictions 2840-39-000-0923
End Users 2840-39-000-0923
- Romania (WR)
Approved Sources 2840-39-000-0923
- Part Number
- Manufacturer
- Status
- NOMIM 4080401025
- Manufacturer
- 0062L - Biroul National De Codificare (Active)
- Definitive Standard
- Definitive Standard
- MOTOR VK-1A (HONG-5)
- 0062L - Biroul National De Codificare (Active)
- Secondary Buy
- Secondary Buy
Similar Supply Items to 2840-39-000-0923
