Rocket Motor

Model / MPN: LD625411 | NSN: 1340-00-443-1511

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

1340-00-443-1511

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

72.260 inches

Size Designation

5 inch

Model Number

Mk 16 mod 3

Motor Propellant Grain Quantity

Motor Propellant Material

Composition n-4 cannon powder

Motor Propellant Grain Model Number

Mk 49 mods

Motor Propellant Grain Weight

34.97 pounds

Cable Assembly Model Number

Not assigned

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Extruded double-base solid

Igniter Model Number

Mk 130 mod 1

Burning Time In Seconds

1.04

Thrust

7500.000 pounds

Straight Section Outside Diameter

5.125 inches

Resonance Rod

Included

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-j247

Dot Registration Code

Ex1988060932

Gross Weight

98.0 shipping container pounds and 2572.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

21.53 pounds

Fsc Application Data

Rocket

LD625 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

LD625411 Cross Reference

4902188
1340-J247