Rocket Motor

Model / MPN: DL1569401 | NSN: 1340-00-969-9464

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

1340-00-969-9464

Sold in multiples of

DEMIL

DEMIL/MLI

Overall Length

76.500 inches

Size Designation

5 inch

Specific Usage Design

Linear demolition charge

Model Number

Mk 22 mod 1

Motor Propellant Grain Quantity

Motor Propellant Material

Solid double base propellant extruded

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 0

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-j144

Dot Registration Code

Ex1988030894

Net Explosive Weight

43.110001 storage pounds and 43.110001 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Supplementary Features

Unit package quantity is 1

Weight

120.00 pounds

DL156 Series Parts

Pricing and Availability

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ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
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7 Year Record Retention
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HAZMAT Certified
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DL1569401 Cross Reference

1340-J144