Rocket Motor

Model / MPN: 1340-J146 | NSN: 1340-01-108-8854

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

1340-01-108-8854

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

41.750 inches

Size Designation

2.75 inch

Specific Usage Design

2.75 inch rocket

Model Number

Mk66

Motor Propellant Grain Quantity

Motor Propellant Material

Ethyl, cellulose

Motor Propellant Grain Model Number

Mk90 mod 0

Motor Propellant Grain Weight

7.0 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Igniter Model Number

Mk125

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-j146

Dot Registration Code

Ex1988100410

Gross Weight

142.0 shipping container pounds and 2201.0 pallet, us army 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 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-J146 Cross Reference

233AS400