Rocket Motor

Model / MPN: M12400 | NSN: 1340-00-038-8437

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

1340-00-038-8437

Sold in multiples of

2 EA

DEMIL

DEMIL/MLI

Overall Length

12.530 inches

Size Designation

5 inch

Model Number

Mk 5 all mods

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

Mk 24 mod 1

Motor Propellant Grain Weight

4.034 pounds

Cable Assembly Model Number

Not assigned

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

External-cruciform, extruded

Igniter Model Number

Mk 120 mod 0, 1 or 2

Burning Time In Seconds

0.97

Thrust

875.000 pounds

Straight Section Outside Diameter

4.947 inches

Nozzle Cant Angle In Deg

12.00

Resonance Rod

Not included

Integral Stabilization Method

Spin

Specific Launcher For Which Designed

Launcher mk 50, 51, 101 and 102

Dod Ammunition Code

1340-j163

Gross Weight

53.7 shipping container pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division and c storage compatibility group and j department of transportation class

Quantity Per Shipping Container

Weight

16.45 pounds

M1240 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.

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M12400 Cross Reference

1340-J163