Rocket Motor

Model / MPN: 1340-J143 | NSN: 1340-00-187-5104

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

1340-00-187-5104

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

76.000 inches

Size Designation

5 inch

Specific Usage Design

Linear demolition charge

Model Number

Mk 22 mod 2

Motor Propellant Grain Quantity

Motor Propellant Material

Solventless double base propellant

Motor Propellant Grain Model Number

Mk 29 mod 1

Motor Propellant Grain Weight

43.4 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

2.30

Thrust

8080.000 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

Dot Registration Code

Ex1988060917

Net Explosive Weight

43.110001 storage pounds and 43.110001 transportation pounds

Gross Weight

191.0 shipping container pounds and 1806.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

120.00 pounds

1340 Series Parts

Pricing and Availability

Send us a request for quote using the form below. Our team will contact you with an up to date pricing and availability quote ASAP.

Certified Quality Assurance

ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
100% Product Inspections
7 Year Record Retention
On Time Delivery
HAZMAT Certified
Worldwide Shipping

1340-J143 Cross Reference

DL2847573