Results of the ASTRO-1 preliminary design review coupled loads analysis are presented. The M6.0Y Generic Shuttle mathematical models were used. Internal accelerations, interface forces, relative displacements, and net e.g., accelerations were recovered for two ASTRO-1 payloads in a tandem configuration. Twenty-seven load cases were computed and summarized. Load exceedences were found and recommendations made.
ASTRO-1 Preliminary Design Review Coupled Load Analysis
1984
881 pages
Report
No indication
English
STS (Astro Missions) Payload Design Load Evolution
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