Rocket Motor

Model / MPN: DL318AS200 | NSN: 1340-00-007-9750

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

1340-00-007-9750

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

76.759 inches

Size Designation

5 inch

Model Number

Mk 71 mod 1

Motor Propellant Grain Quantity

Motor Propellant Grain Model Number

Mk 88 mod 0

Motor Propellant Grain Weight

46.8 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

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

Igniter Model Number

Mk 282 mod 0

Burning Time In Seconds

1.70

Thrust

5500.000 pounds

Straight Section Outside Diameter

5.125 inches

Resonance Rod

Included

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-j271

Dot Registration Code

Ex1988060894

Net Explosive Weight

45.6 storage pounds and 45.6 transportation pounds

Gross Weight

114.5 shipping container pounds and 2748.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

79.50 pounds

318AS 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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DL318AS200 Cross Reference

1340-J271