Rocket Motor

Model / MPN: 2000087 | NSN: 1340-00-093-1065

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

1340-00-093-1065

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

33.450 inches

Model Number

Mk 6 mod 1, 15 ks-1000

Motor Propellant Grain Quantity

Motor Propellant Material

Aeroplex an583af

Motor Propellant Grain Weight

72.0 pounds

Propellant Inhibitor

Included

Igniter

Not included

Propellant Accommodation Type

Solid cylindrical w/tapered ends, longitudinal perforation-longitudinal slot

Burning Time In Seconds

15.00

Thrust

1000.000 pounds

Straight Section Outside Diameter

10.300 inches

Resonance Rod

Not included

Specific Launcher For Which Designed

Not designed for specific launcher

Dod Ammunition Code

1340-h340

Dot Registration Code

Ex1988060905

Gross Weight

2012.0 shipping container pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

72.00 pounds

20000 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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ISO 9001:2015 + AS9120B
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HAZMAT Certified
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2000087 Cross Reference

LD515662
1340-H340
1340-670-0002