Model: 82-6-29

Rocket Motor
Description:

100.100 inches overall length, model tm61 missile specific usage design, xm13/t50/ model number, 1337-v180 dod ammunition code.

Properties:

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
NSN
1337-00-302-1716
Part Number
82-6-29
Description
Rocket Motor
CAGE
18876

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.

Part 82-6-29 NSN 1337-00-302-1716

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
21790
FIIG:
T357-B
Concept No.:
App. Key:
BA
Cond. Code:
2
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
U
ESD:
ESD:
MMAC:
CRITL:
X

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Schedule B and Export
  • Schedule B: 9306900060
  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 336415
  • USDA: 1

Freight Class: Parts for guided missiles

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