Model: 1340-J102

Rocket Motor

Properties:

Overall Length
39.920 inches
Size Designation
2.75 inch
Model Number
Mk 3 mod 1
Motor Propellant Grain Quantity
1
Motor Propellant Material
Ballistite
Motor Propellant Grain Model Number
Mk 43 mod 1
Motor Propellant Grain Weight
6.4 pounds
Cable Assembly Model Number
Not assigned
Propellant Inhibitor
Included
Igniter
Included
Igniter Installation
Installed
Propellant Accommodation Type
Extruded cylinder solid w/internal star-shaped longitudinal cavity
Igniter Model Number
Mk 125 mod 4
Cable Assembly Connector Type
Integral contact
Burning Time In Seconds
1.69
Thrust
7.200 pounds
Straight Section Outside Diameter
2.750 inches
Resonance Rod
Included
Integral Stabilization Method
Fin
Dod Ammunition Code
1340-j102
Weight
6.22 pounds
Reference Number Differentiating Characteristics
As differentiated by unit package quantity, unit package type, package model number
NSN
1340-00-038-8217
Part Number
1340-J102
Description
Rocket Motor
CAGE
99999

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 1340-J102 NSN 1340-00-038-8217

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:
A
ESD:
ESD:
MMAC:
CRITL:
X

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Schedule B and Export
  • Schedule B: 9306900080
  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 332993
  • USDA: 1

Freight Class: Parts for bombs, grenades, torpedos, mines, and similar munitions of war

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