Rocket Motor

Model / MPN: 1340-H303 | NSN: 1340-01-252-0324

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

1340-01-252-0324

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Specific Usage Design

As target

Motor Propellant Grain Quantity

Motor Propellant Material

Aluminum potassium perchlorate powder and ammonium perchlorate

Motor Propellant Grain Weight

62.2 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Dod Ammunition Code

1340-h303

Reference Number Differentiating Characteristics

Asdifferentiated by packaging

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
Worldwide Shipping

1340-H303 Cross Reference

13281000