Rocket Motor

Model / MPN: LD270002 | NSN: 1340-00-768-0640

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

1340-00-768-0640

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

72.260 inches

Size Designation

5 inch

Model Number

Mk 16 mod 0, 1 and 2

Motor Propellant Grain Quantity

Motor Propellant Material

Composition n-4 cannon powder

Motor Propellant Grain Model Number

Mk 49 and mods

Motor Propellant Grain Weight

34.97 pounds

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

Ex1988060941

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

21.53 pounds

LD270 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.

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LD270002 Cross Reference

1517491
657377
LD267989
1340-J247