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Rocket Motor

Model / MPN: 1335AS810 | NSN: 1340-01-325-9195
ITAR Registered seal

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
1340-01-325-9195
Sold in multiples of
1 EA
DEMIL
DEMIL/MLI
Overall Length
15.300 inches
Specific Usage Design
Dgtr-18a is an inert rocket intended to serve as a substitute for live rocket units during maintenance and operational training
Model Number
Dgtr-18a
Motor Propellant Material
Inert material
Igniter
Not included
Straight Section Outside Diameter
2.000 inches
Specific Launcher For Which Designed
Lmu-23b/e or lmu-24b/e
Dod Ammunition Code
1340-h316
Weight
2.20 pounds

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1335AS810 Cross Reference
  • DGTR-18A
  • 1340-H316