Publication Date:
2016-06-07
Description:
The development of an analysis software system capable of performing interdisciplinary preliminary design analyses of large space structure configurations is discussed. Disciplines such as thermal, structures, and controls are to be integrated into a highly user oriented analysis capability. The key feature of the integrated analysis capability, a rapid and efficient system that will minimize solution turnaround time, is discussed.
Keywords:
LAUNCH VEHICLES AND SPACE VEHICLES
Type:
NASA. Langley Res. Center Large Space Systems Technol., 1979; p 383-407
Format:
application/pdf
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