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1337-01-391-6645
Rocket Motor
1337013916645 013916645 704AS4250-2
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 United States
NSN Created on 15 Jun 1994
Data Last Changed
January 2023
January 2023
NATO Update Count
11
11
NATO Data Quality
Marketplace 1337-01-391-6645
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Related Documents 1337-01-391-6645 1+ Documents (More...)
704AS4250-2 A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber
United States (US) 4. 1337-01-391-6645 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1337-01-391-6645 RQST Updated Every Day 1337-01-391-6645 RQST NE Restrictions
United States (US) 4. 1337-01-391-6645 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1337-01-391-6645 RQST Updated Every Day 1337-01-391-6645 RQST NE Restrictions
Restrictions 1337-01-391-6645
Import and Export 1337-01-391-6645
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1337-01-391-6645
- MOE Rule:
- WN01
- Effective Date:
- 1 Nov 1998
- Germany (ZG01)
- Effective Date:
- 1 Jun 1994
- Italy (ZR01)
- Effective Date:
- 1 Dec 2007
- Turkey (ZW01)
- Effective Date:
- 1 Dec 2005
- NATO Maintenance and Supply Agency (ZX01)
- Effective Date:
- 1 Nov 2003
Approved Sources 1337-01-391-6645
- Part Number
- Manufacturer
- Status
- 704AS4250-2
- Manufacturer
- 30003 - Naval Air Systems Command Managed (Active)
- Primary Buy
- Primary Buy
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Freight Information 1337-01-391-6645
1337-01-391-6645 has freight characteristics.. 1337-01-391-6645 has a variance between NMFC and UFC when transported by rail and the description should be consulted.