Rocket Motor

Model / MPN: 1638AS120 | NSN: 1340-01-177-2502

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

1340-01-177-2502

Sold in multiples of

2 EA

DEMIL

DEMIL/MLI

Overall Length

30.630 inches

Model Number

Mk 117 mod 0

Motor Propellant Grain Quantity

Motor Propellant Grain Weight

16.0 pounds

Propellant Inhibitor

Not included

Igniter

Included

Igniter Installation

Installed

Igniter Model Number

Mk 304

Burning Time In Seconds

1.50

Thrust

2500.000 pounds

Straight Section Outside Diameter

5.060 inches

Resonance Rod

Not included

Dod Ammunition Code

1340-h341

Dot Registration Code

Ex1987110637

Net Explosive Weight

16.0534 storage pounds and 16.0534 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

47.50 pounds

1638AS 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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1638AS120 Cross Reference

XSKR821201
1340-H341