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DL639AS4600

Rocket Motor

Model / MPN: DL639AS4600 | NSN: 1337-01-131-7860

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

1337-01-131-7860

Sold in multiples of

DEMIL

DEMIL/MLI

Overall Length

70.000 inches

Specific Usage Design

Natm-9m, aim-9m, guided missile

Model Number

Mk36 mod 9

Motor Propellant Material

X62

Motor Propellant Grain Weight

60.0 pounds

Propellant Inhibitor

Not included

Igniter

Included

Igniter Installation

Installed

Igniter Model Number

Mk297 mod 1

Straight Section Outside Diameter

5.000 inches

Resonance Rod

Not included

Cubic Measure

0.3182 cubic feet

Dod Ammunition Code

1337-v884

Dot Registration Code

Ex1987110574

Net Explosive Weight

60.02 storage pounds and 60.02 transportation pounds

Gross Weight

120.0 shipping container pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Quantity Per Shipping Container

Weight

99.00 pounds

Reference Number Differentiating Characteristics

As differentiated by unit package quantity, unit package type, package model number

639AS 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.

Certified Quality Assurance

ISO 9001:2015 + AS9120B
Counterfeit Parts Prevention
100% Product Inspections
7 Year Record Retention
On Time Delivery
HAZMAT Certified
Worldwide Shipping

DL639AS4600 Cross Reference

1337-V884