Rocket Motor

Model / MPN: 1340-H314 | NSN: 1340-01-356-9873

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

1340-01-356-9873

Sold in multiples of

12 EA

DEMIL

DEMIL/MLI

Overall Length

33.250 inches

Model Number

Mk 128 mod 1

Motor Propellant Grain Weight

65.0 pounds

Igniter

Not included

Igniter Model Number

Mk309

Straight Section Outside Diameter

10.290 inches

Specific Launcher For Which Designed

Jato for c-130 aircraft

Dod Ammunition Code

1340-h314

Dot Registration Code

Ex1998010152

Gross Weight

1960.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

142.00 pounds

Reference Number Differentiating Characteristics

As differentiated by packaging

1340 Series Parts

Pricing and Availability

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Certified Quality Assurance

ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
100% Product Inspections
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HAZMAT Certified
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1340-H314 Cross Reference

1560AS125-2
MK128-1