Rocket Motor

Model / MPN: 233AS500 | NSN: 1340-01-154-1679

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

1340-01-154-1679

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

41.800 inches

Size Designation

2.75 inch

Specific Usage Design

2.75 in. Rocket

Model Number

Mk66-2

Motor Propellant Grain Quantity

Motor Propellant Material

Ethyl, cellulose

Motor Propellant Grain Model Number

Mk 90 mod 0

Motor Propellant Grain Weight

7.1 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Igniter Model Number

Mk125-5

Burning Time In Seconds

1.10

Thrust

1516.000 pounds

Straight Section Outside Diameter

2.750 inches

Integral Stabilization Method

Fin

Package Reference Number

9335618 us army

Dod Ammunition Code

1340-j147

Dot Registration Code

Ex1987080592

Net Explosive Weight

7.12205 storage pounds and 7.12205 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

13.60 pounds

Reference Number Differentiating Characteristics

As differentiated by unit pkg type, unit pkg quantity

233AS Series Parts

Pricing and Availability

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ISO 9001:2015 + AS9120B
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233AS500 Cross Reference

1340-J147