Grain configurations classification for solid propellant rockets by relative web thickness and mean vector direction of burning surface into topological continuum
The morphological continuum in solid propellant grain design
SPACE ENGINEERING, SECOND INTERNATIONAL CONFERENCE ; 1969 ; VENICE, ITALY
01.01.1970
Aufsatz (Konferenz)
Keine Angabe
Englisch
NTIS | 1987
|NTIS | 1988
|Continuum Damage Mechanics Modeling of Solid Propellant
AIAA | 2008
|