A study was performed to quantify the performance of solar thermal power systems for deep space planetary missions. The study incorporated projected advances in solar concentrator and energy conversion technologies. These technologies included inflatable structures, lightweight primary concentrators, high efficiency secondary concentrators, and high efficiency Stirling convertors. Analyses were performed to determine the mass and deployed area of multihundred watt solar thermal power systems for missions out to 40 astronomical units. Emphasis was given to system optimization, parametric sensitivity analyses, and concentrator configuration comparisons. The results indicated that solar thermal power systems are a competitive alternative to radioisotope systems out to 10 astronomical units without the cost or safety implications associated with nuclear sources.
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19 January 2000
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 2000
30 Jan - 3 Feb 2000
Albuquerque, New Mexico (USA)
Research Article|
January 19 2000
Solar Stirling for deep space applications
Lee S. Mason
Lee S. Mason
NASA Glenn Research Center, Cleveland, Ohio 44135
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AIP Conf. Proc. 504, 1272–1277 (2000)
Citation
Lee S. Mason; Solar Stirling for deep space applications. AIP Conf. Proc. 19 January 2000; 504 (1): 1272–1277. https://doi.org/10.1063/1.1290939
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