Rocket Motor

Model / MPN: LD538087 | NSN: 1340-00-896-3695

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

1340-00-896-3695

Sold in multiples of

9 EA

DEMIL

DEMIL/MLI

Overall Length

54.500 inches

Model Number

Mk 7, mod 2, 5ks4500

Motor Propellant Grain Quantity

Motor Propellant Material

Aeroplex an584

Motor Propellant Grain Weight

114.0 pounds

Propellant Inhibitor

Included

Igniter

Not included

Propellant Accommodation Type

Two cylindrical w/longitudinal perforation-one cylindrical solid

Burning Time In Seconds

5.00

Thrust

4500.000 pounds

Straight Section Outside Diameter

9.380 inches

Nozzle Cant Angle In Deg

15.00

Resonance Rod

Included

Dod Ammunition Code

1340-h343

Dot Registration Code

Ex1988030861

Net Explosive Weight

117.5 storage pounds and 117.5 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

111.00 pounds

Reference Number Differentiating Characteristics

As differentiated by igniter

LD538 Series Parts

Pricing and Availability

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LD538087 Cross Reference

2202926
1340-H343