Rocket Motor

Model / MPN: 1340-J104 | NSN: 1340-00-157-6949

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

1340-00-157-6949

Sold in multiples of

DEMIL

DEMIL/MLI

Overall Length

39.340 inches

Size Designation

2.75 inch

Specific Usage Design

2.75 in. Rocket

Motor Propellant Grain Quantity

Motor Propellant Material

Ammonium perchlorate-polysulfide

Motor Propellant Grain Model Number

1148155-1

Motor Propellant Grain Weight

8.3 pounds

Propellant Inhibitor

Not included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Solid

Straight Section Outside Diameter

2.750 inches

Integral Stabilization Method

Fin

Criticality Code Justification

Exwt

Dod Ammunition Code

1340-j104

Dot Registration Code

Ex1988090247

Net Explosive Weight

8.3 storage pounds and 8.3 transportation pounds

Gross Weight

131.0 shipping container pounds

Dot Hazard Class/division

1.3

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

1340 Series Parts

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.

Certified Quality Assurance

ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
100% Product Inspections
7 Year Record Retention
On Time Delivery
HAZMAT Certified
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1340-J104 Cross Reference

SR105AJ1
1148178