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36-38-57

Rocket Motor

Model / MPN: 36-38-57 | NSN: 1337-00-912-3644

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

1337-00-912-3644

Sold in multiples of

DEMIL

DEMIL/MLI

Overall Length

6.330 inches

Specific Usage Design

Model no. Lgm-30 guided missile

Model Number

Ysr59-ar-1

Motor Propellant Grain Quantity

Motor Propellant Material

Arcite 377a

Motor Propellant Grain Weight

0.07 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Extruded single-base solid

Burning Time In Seconds

0.050

Thrust

31.500 pounds

Straight Section Outside Diameter

1.250 inches

Resonance Rod

Not included

Specific Launcher For Which Designed

Not designed for specific launcher

Dod Ammunition Code

1337-v211

Dot Registration Code

Ex1988090188

Net Explosive Weight

0.0706 storage pounds and 0.0706 transportation pounds

Gross Weight

3.0 shipping container pounds and 80030.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

0.70 pounds

Fsc Application Data

Rocket motor, guided missile, explosive loaded

Pricing and Availability

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36-38-57 Cross Reference

331121-1
1337-V211