Model: 1340-J143

Rocket Motor

Properties:

Overall Length
76.000 inches
Size Designation
5 inch
Specific Usage Design
Linear demolition charge
Model Number
Mk 22 mod 3
Motor Propellant Grain Quantity
1
Motor Propellant Material
Solventless double base propellant
Motor Propellant Grain Model Number
N5
Motor Propellant Grain Weight
45.0 pounds
Cable Assembly Model Number
Not assigned
Propellant Inhibitor
Included
Igniter
Included
Igniter Installation
Installed
Propellant Accommodation Type
Internal star, extruded
Igniter Model Number
Mk 275 mod 1
Cable Assembly Connector Type
Jack plug
Burning Time In Seconds
2.50
Thrust
3700.000 pounds
Straight Section Outside Diameter
5.000 inches
Resonance Rod
Not included
Specific Launcher For Which Designed
Demolition kit, m125, m126
Dod Ammunition Code
1340-j143
Weight
120.000 pounds
Reference Number Differentiating Characteristics
As differentiated by unit package quantity, unit package type, motor propellant grain model number, motor propellant grain weight, thrust
NSN
1340-01-114-2313
Part Number
1340-J143
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-J143 NSN 1340-01-114-2313

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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