Solar dynamic space power system heat rejectionA radiator system concept is described that meets the heat rejection requirements of the NASA Space Station solar dynamic power modules. The heat pipe radiator is a high-reliability, high-performance approach that is capable of erection in space and is maintainable on orbit. Results are present of trade studies that compare the radiator system area and weight estimates for candidate advanced high performance heat pipes. The results indicate the advantages of the dual-slot heat pipe radiator for high temperature applications as well as its weight-reduction potential over the range of temperatures to be encountered in the solar dynamic heat rejection systems.
Document ID
19870030901
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlson, A. W. (Grumman Aerospace Corp. Bethpage, NY, United States)
Gustafson, E. (Grumman Aerospace Corp. Bethpage, NY, United States)
Mclallin, K. L. (NASA Lewis Research Center Cleveland, OH, United States)