Shock initiation and detonation behavior of an HMX/AP/Al rocket propellant were studied for nonideal character. Low detonation velocities and unusual shock initiation behavior were observed. Failure to propagate steady detonation in cylinders of the propellant was also noted. (ERA citation 06:019166)
Nonideal Detonation and Initiation Behavior of a Composite Solid Rocket Propellant
1981
5 pages
Report
No indication
English
Laser initiation of solid propellant rocket ignition
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