Rocket Motor

Model / MPN: LD546627 | NSN: 1340-00-042-9271

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

1340-00-042-9271

Sold in multiples of

DEMIL

DEMIL/MLI

Overall Length

21.380 inches

Model Number

Mk 34 mod 1

Motor Propellant Grain Quantity

Motor Propellant Material

Composition n-5

Motor Propellant Grain Model Number

Mk 74 mod 0

Motor Propellant Grain Weight

9.5 pounds

Cable Assembly Model Number

Not assigned

Propellant Inhibitor

Not included

Igniter

Included

Igniter Installation

Installed

Igniter Model Number

Mk 263 mod 1

Cable Assembly Connector Type

Two-prong special

Burning Time In Seconds

0.70

Thrust

2650.000 pounds

Straight Section Outside Diameter

5.380 inches

Resonance Rod

Not included

Dod Ammunition Code

1340-j149

Dot Registration Code

Ex1988030766

Net Explosive Weight

9.0193 storage pounds and 9.0193 transportation pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

27.10 pounds

LD546 Series Parts

Pricing and Availability

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LD546627 Cross Reference

2434633
1340-J149