Premium Information is available for this item - Upgrade for $1 a day

1337-00-302-1716

Rocket Motor

1337003021716 003021716 XM13 82-6-29 1337-V180

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

1337-00-302-1716 ROCKET MOTOR 1337003021716 003021716

Managed by United States
NSN Created on 1 Jan 1960
Data Last Changed
January 2023
NATO Update Count
16
NATO Data Quality
1337-00-302-1716 ROCKET MOTOR 1337003021716 003021716 1/1
NSN 1337-00-302-1716 (Generic Image) 1/1

1337-00-302-1716 Stock and Availability Marketplace 1337-00-302-1716

Need Help?
Request a Quotation from participating marketplace vendors

1337-00-302-1716 Related Documents Related Documents 1337-00-302-1716 1+ Documents (More...)

XM13 82-6-29 1337-V180 A nonairbreathing reaction propulsion device that consists essentially of a thrust
United States (US) 4. 1337-00-302-1716 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 1337-00-302-1716

1337-00-302-1716 Demil Restrictions 1337-00-302-1716

DEMIL: G | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

1337-00-302-1716 is a Rocket Motor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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. The precious metals content of this item is unknown.

1337-00-302-1716 HTS and ScheduleB Import and Export 1337-00-302-1716

1337-00-302-1716 End Users End Users 1337-00-302-1716

MOE Rule:
WN01
Effective Date:
1 Feb 2006
Italy (ZR01)
Effective Date:
1 Apr 1991

1337-00-302-1716 Manufacturers Approved Sources 1337-00-302-1716

1337-00-302-1716 Technical Data Datasheet 1337-00-302-1716

Characteristic
Specifications
FIIG
T357-B
Dod Ammunition Code [DDAC]
1337-V180
Cable Assembly Connector Type [AWBK]
An
Cable Assembly Model Number [ATSP]
Not Assigned
Igniter Installation [AWBG]
Not Installed
Igniter Model Number [AWBJ]
T40
Igniter [AWBF]
Included
Model Number [AMWN]
Xm13/T50/
Motor Propellant Grain Model Number [ATSJ]
T16
Motor Propellant Grain Quantity [ATSG]
12
Motor Propellant Grain Weight [ATSK]
708.0 Pounds
Motor Propellant Material [ATSH]
Ballistite
Nominal Burning Time In Seconds [AWBL]
2.40
Nominal Thrust [AWBM]
57000.000 Pounds
Propellant Accommodation Type [AWBH]
Extruded Double-Base Solid
Propellant Inhibitor [AWBE]
Not Included
Resonance Rod [AWBQ]
Included
Overall Length [ABHP]
100.100 Inches Nominal
Weight [WGHT]
967.00 Pounds
Specific Usage Design [ALXZ]
Model Tm61 Missile
Straight Section Outside Diameter [AWBN]
21.250 Inches Nominal

1337-00-302-1716 Related Items NATO Stock Numbers Related to 1337-00-302-1716

1337-00-302-1716 Freight Data Freight Information 1337-00-302-1716

1337-00-302-1716 has freight characteristics.. 1337-00-302-1716 has a variance between NMFC and UFC when transported by rail and the description should be consulted.