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Worldwide distributor of NSN parts and consumables located in the USA.

Rocket Motor

Model / MPN: 82-6-29 | NSN: 1337-00-302-1716
ITAR Registered seal

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.

Product Details
NATO Stock Number
1337-00-302-1716
Sold in multiples of
DEMIL
DEMIL/MLI
Overall Length
100.100 inches
Specific Usage Design
Model tm61 missile
Model Number
Xm13/t50/
Motor Propellant Grain Quantity
12
Motor Propellant Material
Ballistite
Motor Propellant Grain Model Number
T16
Motor Propellant Grain Weight
708.0 pounds
Cable Assembly Model Number
Not assigned
Propellant Inhibitor
Not included
Igniter
Included
Igniter Installation
Not installed
Propellant Accommodation Type
Extruded double-base solid
Igniter Model Number
T40
Cable Assembly Connector Type
An
Burning Time In Seconds
2.40
Thrust
57000.000 pounds
Straight Section Outside Diameter
21.250 inches
Resonance Rod
Included
Dod Ammunition Code
1337-v180
Weight
967.00 pounds

Pricing and Availability

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82-6-29 Cross Reference
  • XM13
  • 1337-V180