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1337-01-190-8567

Rocket Motor

1337011908567 011908567 4900026-2 1337-V912

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

1337-01-190-8567 ROCKET MOTOR 1337011908567 011908567

Managed by United States
NSN Created on 3 Oct 1984
Data Last Changed
January 2023
NATO Update Count
16
NATO Data Quality
1337-01-190-8567 ROCKET MOTOR 1337011908567 011908567 1/1
NSN 1337-01-190-8567 (Generic Image) 1/1

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1337-01-190-8567 Related Documents Related Documents 1337-01-190-8567 5+ Documents (More...)

4900026-2 1337-V912 A nonairbreathing reaction propulsion device that consists essentially of a thrust
United States (US) 4. 1337-01-190-8567 Marketplace Restrictions Approved Sources Datasheet Management
Restrictions 1337-01-190-8567 DEMIL: G | DEMILI : | CRITICALITY : X | HMIC : N | PMIC : A | EDC
Fluid Filter Element 4330143898158143898158 4900026 https//www.nsnlookup.com /fsg-13/fsc-1337/us 1337-01-190-8567
Rocket Motor 1337011908567 011908567 Upgrade for $1 a day Upgrade your Account Upgrade 1337-01-
190-8567Rocket Motor1337011908567 011908567 4900026 Restrictions 1005-12-169-6769 DEMIL: | DEMILI : |
enable JavaScript in your web browser . 4330-14-389 https//www.nsnlookup.com /fsg-13/fsc-1337/us 1337-01-190-8567
Rocket Motor 1337011908567 011908567 Upgrade for $1 a day Upgrade your Account Upgrade 1337-01-
190-8567Rocket Motor1337011908567 011908567 4900026 Restrictions 4330-14-389-8158 DEMIL: | DEMILI : |
272-2363 Guided Missile Sustainer Section A/B44G-1 GRAYRNCC: 5 | RNVC: 1 | DAC: 5 5 Feb 1988 1337-01-190-8567
Explosive Propulsion Units, Solid Fuel; and Components from United States (US) DAC: 5 5 Feb 1988 1337-01-190-8567

1337-01-190-8567 Demil Restrictions 1337-01-190-8567

DEMIL: G | DEMILI: | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

1337-01-190-8567 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 Ammunition or Explosive and is a US Munitions List or Commerce Control List Item where demilitarization is required. This item is not suspected to be hazardous. This item does not contain a precious metal.

1337-01-190-8567 HTS and ScheduleB Import and Export 1337-01-190-8567

1337-01-190-8567 End Users End Users 1337-01-190-8567

MOE Rule:
WN01
Effective Date:
1 Nov 1998

1337-01-190-8567 Manufacturers Approved Sources 1337-01-190-8567

1337-01-190-8567 Technical Data Datasheet 1337-01-190-8567

Characteristic
Specifications
FIIG
T357-B
Dod Ammunition Code [DDAC]
1337-V912
Dot Registration Code [DTRC]
Ex1987110594
Cable Assembly Connector Type [AWBK]
An
Cable Assembly Model Number [ATSP]
Dwg2623586
Fsc Application Data [ZZZV]
Guided Missile
Gross Weight [GRWT]
1654.0 Pallet Pounds
Hazardous Material Classification Code [HMCC]
1.3 Department Of Defense Hazard Class Division
Igniter Installation [AWBG]
Installed
Igniter Model Number [AWBJ]
Mk265 Mod 0
Igniter [AWBF]
Included
Model Number [AMWN]
Mk39 Mod 9
Net Explosive Weight [EXWT]
94.199997 Storage Pounds And 94.199997 Transportation Pounds
Propellant Inhibitor [AWBE]
Included
Quantity Per Shipping Container [QTSC]
1
Reference Number Differentiating Characteristics [ZZZY]
As Differentiated By Unit Package Quantity,Unit Package Type,Package Model Number
Resonance Rod [AWBQ]
Not Included
Overall Length [ABHP]
51.800 Inches Nominal
Weight [WGHT]
157.40 Pounds
Straight Section Outside Diameter [AWBN]
8.000 Inches Nominal

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1337-01-190-8567 Freight Data Freight Information 1337-01-190-8567

1337-01-190-8567 has freight characteristics.. 1337-01-190-8567 has a variance between NMFC and UFC when transported by rail and the description should be consulted.