Rocket Motor

Model / MPN: 53A85A | NSN: 1340-00-093-1067

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

1340-00-093-1067

Sold in multiples of

6 EA

DEMIL

DEMIL/MLI

Overall Length

54.310 inches

Model Number

Mk 7 mod 1, 5ks4500

Motor Propellant Grain Quantity

Motor Propellant Material

Aeroplex an584

Motor Propellant Grain Weight

114.0 pounds

Propellant Inhibitor

Included

Igniter

Not included

Propellant Accommodation Type

Two cylindrical w/longitudinal perforation-one cylindrical solid

Burning Time In Seconds

5.00

Thrust

4500.000 pounds

Straight Section Outside Diameter

9.380 inches

Nozzle Cant Angle In Deg

30.00

Resonance Rod

Included

Integral Thrust Direction Control Method

Jet vane

Dod Ammunition Code

1340-h345

Dot Registration Code

Ex1988030777

Net Explosive Weight

117.5 storage pounds and 117.5 transportation pounds

Gross Weight

2531.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

111.00 pounds

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

53A85A Cross Reference

1340-H345