Thermal control requirements for large space structuresPerformance capabilities and weight requirements of large space structure systems will be significantly influenced by thermal response characteristics. Analyses have been performed to determine temperature levels and gradients for structural configurations and elemental concepts proposed for advanced system applications ranging from relatively small, low-power communication antennas to extremely large, high-power Satellite Power Systems (SPS). Results are presented for selected platform configurations, candidate strut elements, and potential mission environments. The analyses also incorporate material and surface optical property variation. The results illustrate many of the thermal problems which may be encountered in the development of three systems.
Document ID
19780068090
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Manoff, M. (Rockwell International Corp. Downey, Calif., United States)