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1337-00-411-7050
Rocket Motor
1337004117050 004117050 01A00063-043
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
January 2023
15
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Restrictions 1337-00-411-7050
1337-00-411-7050 is a Rocket Motor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List or Commerce Control List Item where the Item Manager, Equipment Specialist or Product Specialist must provide special demilitarization instructions. This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 1337-00-411-7050
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1337-00-411-7050
- MOE Rule:
- WN01
- Effective Date:
- 1 Feb 2006
Approved Sources 1337-00-411-7050
- Part Number
- Manufacturer
- Status
- 01A00063-043
- Manufacturer
- 10396 - Hercules Inc (Obsolete)
- Original Design
- Original Design
Datasheet 1337-00-411-7050
- Characteristic
- Specifications
- FIIG
- Specifications
- T357-B
- Dot Registration Code [DTRC]
- Ex1988100978
- Hazardous Material Classification Code [HMCC]
- 1.1 Department Of Defense Hazard Class Division
- Overall Length [ABHP]
- 85.260 Inches Nominal
- Specific Usage Design [ALXZ]
- Lgm-30 Guided Missile
- Straight Section Outside Diameter [AWBN]
- 37.900 Inches Nominal
NATO Stock Numbers Related to 1337-00-411-7050
Freight Information 1337-00-411-7050
1337-00-411-7050 has freight characteristics.. 1337-00-411-7050 has a variance between NMFC and UFC when transported by rail and the description should be consulted.