Rocket Motor

Model / MPN: 1340-H340 | NSN: 1340-00-309-5092

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

1340-00-309-5092

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

33.450 inches

Model Number

Mk 6 mod 1

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 slot

Burning Time In Seconds

15.00

Thrust

1000.000 pounds

Straight Section Outside Diameter

10.300 inches

Resonance Rod

Not included

Package Reference Number

1168as100 us navy

Dod Ammunition Code

1340-h340

Dot Registration Code

Ex1988090255

Gross Weight

186.0 shipping container pounds and 1776.0 pallet domestic, us navy pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Shipping Container Quantity Per Pallet

9 navy pallet domestic

Weight

72.00 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.

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ISO 9001:2015 + AS9120B
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1340-H340 Cross Reference

2000087