1340-15-118-2947
Rocket Motor
1340151182947 151182947 BPD 3.1.0.0605.0
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 Italy
NSN Created on 4 May 1994
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1340-15-118-2947
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Related Documents 1340-15-118-2947 2+ Documents (More...)
BPD 3.1.0.0605.0 A nonairbreathing reaction propulsion device that consists essentially of a thrust
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RQST NE Updated Every Day 1340-15-118-2947 RQST Updated Every Day 1340-15-118-2947 RQST NE Restrictions
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RQST NE Updated Every Day 1340-15-118-2947 RQST Updated Every Day 1340-15-118-2947 RQST NE Restrictions
DAC: 5 10 Oct 1996 1340-15-130-3307 Razzo TIP0ARF8M2PIRNCC: 3 | RNVC: 2 | DAC: 5 9 Oct 1996 1340-15-118-2947
Restrictions 1340-15-118-2947
End Users 1340-15-118-2947
- Italy (ZR)
Approved Sources 1340-15-118-2947
- Part Number
- Manufacturer
- Status
- BPD 3.1.0.0605.0
- Manufacturer
- A3313 - Avio Spa (Active)
- Primary Buy
- Primary Buy
- BPD 3.1.0.0605.0
- A3460 - Ge Avio Srl (Active)
- Primary Buy
- Primary Buy
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