1340-12-910-0512
Rocket Motor
1340129100512 129100512 1AL1300471 M261 JB59 DM14
A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber and exhaust nozzle, and that carries its own solid oxidizer-fuel combination from which hot gases are generated by combustion and expanded through a nozzle. See also ROCKET MOTOR CLUSTER. View more Rocket Motor
Managed by Germany
NSN Created on 30 May 1969
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
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1AL1300471 M261 JB59 DM14 A nonairbreathing reaction propulsion device that consists essentially of
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Restrictions 1340-12-910-0512
Approved Sources 1340-12-910-0512
- Part Number
- Manufacturer
- Status
- 1AL1300471
- Manufacturer
- D1839 - Baainbw Dokumente Ohne (Active)
- Definitive Standard
- Definitive Standard
- M261
- B0139 - Thales Belgium (Active)
- Secondary Buy
- Secondary Buy
- JB59
- D5000 - Baainbw K1.1-Munitionsaustauschkode (Active)
- NATO Reference
- NATO Reference
- DM14
- D2000 - Baainbw K1.1-Deutsches (Active)
- NATO Reference
- NATO Reference
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