Rocket Motor

Model / MPN: 3028460 | NSN: 1340-00-316-3648

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

1340-00-316-3648

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

70.059 inches

Size Designation

5 inch

Model Number

Mk 81 mod 0

Motor Propellant Grain Quantity

Motor Propellant Material

Nitrocellulose

Motor Propellant Grain Model Number

Mk 49 mod 1

Motor Propellant Grain Weight

33.5 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Double base

Igniter Model Number

Mk 282 mod 0

Burning Time In Seconds

1.20

Straight Section Outside Diameter

5.125 inches

Resonance Rod

Not included

Dod Ammunition Code

1340-j272

Dot Registration Code

Ex1988060924

Net Explosive Weight

33.59 storage pounds and 33.59 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

101.85 pounds

30284 Series Parts

Pricing and Availability

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ISO 9001:2015 + AS9120B
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3028460 Cross Reference

DL3028460
1340-J272