Rocket Motor

Model / MPN: 1340-H308 | NSN: 1340-01-266-8120

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

1340-01-266-8120

Sold in multiples of

4 EA

DEMIL

DEMIL/MLI

Overall Length

41.828 inches

Size Designation

2.75 inch

Model Number

Mk 66

Motor Propellant Grain Quantity

Motor Propellant Material

Inert material

Motor Propellant Grain Model Number

Mk 90 mod 0

Motor Propellant Grain Weight

7.6 pounds

Propellant Inhibitor

Not included

Igniter

Not included

Igniter Installation

Not installed

Straight Section Outside Diameter

2.750 inches

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-h308

Gross Weight

74.0 shipping container pounds

Quantity Per Shipping Container

Weight

13.60 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-H308 Cross Reference

233AS431