Rocket Motor

Model / MPN: 1340-J145 | NSN: 1340-01-097-6365

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

1340-01-097-6365

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

52.000 inches

Package Model Number

Mk 4 mod 1

Specific Usage Design

Test vehicles, sleds and drones

Model Number

Mk23 mod 2

Motor Propellant Grain Quantity

Motor Propellant Grain Weight

108.0 pounds

Propellant Inhibitor

Included

Igniter

Not included

Propellant Accommodation Type

Solid cylindrical w/longitudinal perforation

Igniter Model Number

Mk296 mod 0

Burning Time In Seconds

2.20

Thrust

11000.000 pounds

Straight Section Outside Diameter

10.000 inches

Resonance Rod

Not included

Dod Ammunition Code

1340-j145

Dot Registration Code

Ex1988030908

Gross Weight

2565.0 shipping container pounds and 2565.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

244.00 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-J145 Cross Reference

1255AS100