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1131AS200-1

Rocket Motor

Model / MPN: 1131AS200-1 | NSN: 1337-01-150-7939

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

1337-01-150-7939

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

59.600 inches

Specific Usage Design

Aim-7f, -7m, -7p guided missile

Model Number

Mk58 mod 5

Motor Propellant Material

Kaa-114

Motor Propellant Grain Weight

133.3 pounds

Cable Assembly Model Number

Not assigned

Propellant Inhibitor

Not included

Igniter

Included

Igniter Installation

Installed

Igniter Model Number

P/n2824894

Cable Assembly Connector Type

Two-prong special

Straight Section Outside Diameter

8.000 inches

Resonance Rod

Not included

Cubic Measure

1.7337 cubic feet

Dod Ammunition Code

1337-v378

Dot Registration Code

Ex1987110579

Net Explosive Weight

133.300003 storage pounds and 133.300003 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

210.80 pounds

Reference Number Differentiating Characteristics

As differentiated by unit package quantity, unit package type, package model number

1131AS200 Series Parts

1131AS200-1

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
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1131AS200-1 Cross Reference

1337-V378