Rocket Motor

Model / MPN: 1340-J102 | NSN: 1340-00-309-5102

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

1340-00-309-5102

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

39.920 inches

Size Designation

2.75 inch

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

Mk43 all mods

Motor Propellant Grain Weight

6.40 pounds

Cable Assembly Model Number

Mk 3 andmods

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

Extruded cylinder solid w/internal star-shaped longitudinal cavity

Igniter Model Number

Mk 125 mod 2

Cable Assembly Connector Type

Integral contact

Burning Time In Seconds

1.69

Thrust

7.200 pounds

Straight Section Outside Diameter

22.250 inches

Resonance Rod

Included

Integral Stabilization Method

Fin

Dod Ammunition Code

1340-j102

Net Explosive Weight

6.4 transportation pounds

Gross Weight

131.0 shipping container pounds

Quantity Per Shipping Container

Weight

6.22 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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1340-J102 Cross Reference

S9T0A