Rocket Motor

Model / MPN: 1340-H317 | NSN: 1340-01-331-5694

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

1340-01-331-5694

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

57.270 inches

Model Number

Mk129 mod 0

Motor Propellant Grain Weight

135.00 pounds

Igniter

Included

Igniter Model Number

Mk310

Straight Section Outside Diameter

11.390 inches

Specific Launcher For Which Designed

Jato for unmaned aerial vehicle, medium range target

Dod Ammunition Code

1340-h317

Hazardous Material Classification Code

Ii-b coast guard class and 1.3 department of defense hazard class division and j department of transportation class and iii firefighting group and c storage compatibility group

Weight

285.00 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.

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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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1340-H317 Cross Reference

MK129-0
590-174-0030