Rocket Motor

Model / MPN: MILJ12823 | NSN: 1340-00-028-6133

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

1340-00-028-6133

Sold in multiples of

DEMIL

DEMIL/MLI

Overall Length

21.500 inches

Model Number

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

M16

Motor Propellant Grain Weight

9.17 pounds

Cable Assembly Model Number

Not assigned

Propellant Inhibitor

Not included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Extruded double-base solid

Igniter Model Number

M21

Cable Assembly Connector Type

Two-prong special

Burning Time In Seconds

0.70

Thrust

2650.000 pounds

Straight Section Outside Diameter

5.120 inches

Resonance Rod

Not included

Dod Ammunition Code

1340-h305

Weight

17.93 pounds

MILJ1 Series Parts

Pricing and Availability

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MILJ12823 Cross Reference

82-6-24
ES2650
1340-H305