Advances in Stress Analysis of Solid Propellant Rocket Grains.
ROHM AND HAAS CO HUNTSVILLE AL REDSTONE RESEARCH LABS
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A computer program for the elastic stress analysis of solid propellant grains encased in orthotropic, elastic motor cases is given. This program is similar to a previously published program AMG032 but incorporates refinements in input procedures and solution techniques developed over several years. Present computational times are approximately 40 less than those experienced with AMG032. Author
- Solid Rocket Propellants