Rocket Motor

Model / MPN: 1340-J161 | NSN: 1340-00-038-8431

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

1340-00-038-8431

Sold in multiples of

2 EA

DEMIL

DEMIL/MLI

Overall Length

22.650 inches

Size Designation

5 inch

Model Number

Mk 3 all mods

Motor Propellant Grain Quantity

Motor Propellant Material

Ballistite

Motor Propellant Grain Model Number

Mk 21 mod 2

Motor Propellant Grain Weight

10.32 pounds

Cable Assembly Model Number

Not assigned

Propellant Inhibitor

Included

Igniter

Included

Igniter Installation

Installed

Propellant Accommodation Type

External-cruciform, extruded

Igniter Model Number

Mk 117 mod 0, 1 or 2

Burning Time In Seconds

1.07

Thrust

2080.000 pounds

Straight Section Outside Diameter

4.947 inches

Nozzle Cant Angle In Deg

12.00

Resonance Rod

Not included

Integral Stabilization Method

Spin

Specific Launcher For Which Designed

Launcher mk 50, 51 101 and 102

Dod Ammunition Code

1340-j161

Dot Registration Code

Ex1988030739

Net Explosive Weight

10.016 storage pounds and 10.016 transportation pounds

Gross Weight

78.7 shipping container pounds and 1450.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

22.20 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-J161 Cross Reference

467046