Rocket Motor

Model / MPN: 1340-J106 | NSN: 1340-00-953-8924

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

1340-00-953-8924

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

39.913 inches

Size Designation

2.75 inch

Model Number

Mk 40 mod 1, 2, 3

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

Mk 43 mods

Motor Propellant Grain Weight

5.9 pounds

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Extruded double-base solid

Igniter Model Number

Mk 125 mod 4

Burning Time In Seconds

1.69

Thrust

720.000 pounds

Straight Section Outside Diameter

2.800 inches

Nozzle Cant Angle In Deg

24.00

Resonance Rod

Included

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-j106

Dot Registration Code

Ex1988030893

Net Explosive Weight

6.0222 storage pounds and 6.0222 transportation pounds

Gross Weight

122.0 shipping container pounds and 1574.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

12.67 pounds

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-J106 Cross Reference

1517506