1338-14-386-1767
Rocket Motor Exhaust Nozzle
1338143861767 143861767 15601308
An item designed with a constricting throat section and a divergent section. The constricting throat section compresses the propellant gases and maintains the pressure within the thrust chamber of the rocket motor by limiting the flow of gases. The divergent section controls the expansion of the gases causing increased thrust. View more Rocket Motor Exhaust Nozzle
Managed by France
NSN Created on 24 Aug 1983
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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15601308 An item designed with a constricting throat section and a divergent section.
Request a Quotation from participating marketplace vendors Request Updated Every Day 1338-14-386-1767
RQST NE Updated Every Day 1338-14-386-1767 RQST Updated Every Day 1338-14-386-1767 RQST NE Restrictions
Request a Quotation from participating marketplace vendors Request Updated Every Day 1338-14-386-1767
RQST NE Updated Every Day 1338-14-386-1767 RQST Updated Every Day 1338-14-386-1767 RQST NE Restrictions
AMG175825RNCC: 3 | RNVC: 2 | DAC: 2 16 Dec 1986 1338-14-279-5540 1338-14-278-9227 1338-14-305-7198 1338-14-386-1767
Restrictions 1338-14-386-1767
End Users 1338-14-386-1767
- France (ZF)
Approved Sources 1338-14-386-1767
- Part Number
- Manufacturer
- Status
- 15601308
- Manufacturer
- F0555 - Mbda France (Active)
- Primary Buy
- Primary Buy
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