Rocket Motor

Model / MPN: DL318AS100 | NSN: 1340-00-148-1130

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

1340-00-148-1130

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

76.260 inches

Size Designation

5 inch

Model Number

Mk 71 mod 0

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

Mk 49 mods

Motor Propellant Grain Weight

34.9 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Extruded double-base solid w/internal star-shaped longitudinal cavity

Igniter Model Number

Mk 282 mod 0

Burning Time In Seconds

1.04

Thrust

7500.000 pounds

Straight Section Outside Diameter

5.125 inches

Resonance Rod

Included

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-j270

Dot Registration Code

Ex1988060914

Net Explosive Weight

35.126999 storage pounds and 35.126999 transportation pounds

Gross Weight

101.8 shipping container pounds and 2594.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

66.85 pounds

318AS Series Parts

Pricing and Availability

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ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
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7 Year Record Retention
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HAZMAT Certified
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DL318AS100 Cross Reference

1340-J270