Solid propellant grain design and charge configuration, reviewing dendrite, wagonwheel, star, slotted, conocyl and finocyl grains
The morphological continuum in solid propellant grain design.
CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION ; 1968 ; NEW YORK, NY
1968-10-01
Conference paper
No indication
English
NTIS | 1987
|NTIS | 1988
|Continuum Damage Mechanics Modeling of Solid Propellant
AIAA | 2008
|