Rocket Motor

Model / MPN: LD268439 | NSN: 1340-00-038-8444

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

1340-00-038-8444

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

52.780 inches

Size Designation

5 inch

Model Number

Mk 10 mod 6

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

Mk 18 all mods

Motor Propellant Grain Weight

24.83 pounds

Cable Assembly Model Number

Mk 11 mod 4

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

External-cruciform, extruded

Igniter Model Number

Mk114 mod 0 or 1

Cable Assembly Connector Type

Jack plug

Burning Time In Seconds

1.15

Thrust

4700.000 pounds

Straight Section Outside Diameter

5.000 inches

Resonance Rod

Not included

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-j165

Dot Registration Code

Ex1988030745

Net Explosive Weight

24.121 storage pounds and 24.121 transportation pounds

Gross Weight

122.0 shipping container pounds and 2540.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

62.33 pounds

LD268 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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ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
100% Product Inspections
7 Year Record Retention
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HAZMAT Certified
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LD268439 Cross Reference

656724
1340-J165