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R47627-517

Rocket Motor

Model / MPN: R47627-517 | NSN: 1337-00-232-4187

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

1337-00-232-4187

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Length

40.140 inches

Specific Usage Design

Agm-65a, guided missile

Model Number

Sr109-tc-1

Motor Propellant Grain Weight

60.7 pounds

Igniter

Included

Igniter Installation

Installed

Straight Section Outside Diameter

10.650 inches

Criticality Code Justification

Exwt

Dod Ammunition Code

1337-v278

Dot Registration Code

Ex1988100971

Net Explosive Weight

64.699997 storage pounds and 64.699997 transportation pounds

Gross Weight

165.0 shipping container pounds

Dot Hazard Class/division

1.3

Hazardous Material Classification Code

1.3 department of defense hazard class division and c storage compatibility group

Quantity Per Shipping Container

Weight

100.00 pounds

R47627 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

R47627-517 Cross Reference

3102309-4-1
3102309-2-1
3102309-4-2
3102309-4-3
SR109-TC-1
R47627-514
1337-V278