Rocket Motor

Model / MPN: LD537844 | NSN: 1340-00-806-3408

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

1340-00-806-3408

Sold in multiples of

9 EA

DEMIL

DEMIL/MLI

Overall Length

55.000 inches

Model Number

Mk 25 mod 1

Motor Propellant Grain Quantity

Motor Propellant Material

Ammonium perchlorate

Motor Propellant Grain Model Number

Mk 66 mod 0

Motor Propellant Grain Weight

121.9 pounds

Propellant Inhibitor

Not included

Igniter

Not included

Propellant Accommodation Type

Solid cylindrical w/longitudinal perforation

Burning Time In Seconds

5.00

Thrust

4500.000 pounds

Straight Section Outside Diameter

9.740 inches

Nozzle Cant Angle In Deg

30.00

Resonance Rod

Not included

Dod Ammunition Code

1340-h342

Dot Registration Code

Ex1988030852

Gross Weight

2270.0 pallet pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

205.24 pounds

LD537 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

LD537844 Cross Reference

2205571
1340-H342