Rocket Motor

Model / MPN: 233AS500-1 | NSN: 1340-01-416-1878

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

1340-01-416-1878

Sold in multiples of

4 EA

DEMIL

DEMIL/MLI

Overall Length

41.750 inches

Size Designation

2.75 inch

Motor Propellant Grain Quantity

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

Mk 66 mod 2

Straight Section Outside Diameter

2.750 inches

Integral Stabilization Method

Fin

Package Reference Number

233as424 us navy

Dod Ammunition Code

1340-ha03

Dot Registration Code

Ex1987080595a

Net Explosive Weight

7.12205 storage pounds and 7.12205 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

233AS500 Series Parts

Pricing and Availability

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Rocket Motor

Pricing and Availability

Certified Quality Assurance

233AS500-1 Cross Reference