Rocket Motor

Model / MPN: 1340-H343 | NSN: 1340-01-292-2874

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

1340-01-292-2874

Sold in multiples of

9 EA

DEMIL

DEMIL/MLI

Overall Length

51.000 inches

Model Number

Mk7 mod 4

Motor Propellant Grain Quantity

Motor Propellant Material

Carboxl terminated polybutadine acrylonitrile and ammonium perchlorate

Motor Propellant Grain Weight

106.0 pounds

Burning Time In Seconds

5.00

Thrust

4500.000 pounds

Straight Section Outside Diameter

9.400 inches

Nozzle Cant Angle In Deg

15.0

Dod Ammunition Code

1340-h343

Dot Registration Code

Ex1987110651

Gross Weight

2531.0 shipping container pounds

Hazardous Material Classification Code

1.3 department of defense hazard class division

Weight

220.00 pounds

1340 Series Parts

Pricing and Availability

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1340-H343 Cross Reference

MK7-4
1638AS147