The electronic and other payload power densities in future micro/nano spacecraft are expected to exceed 25 Watts/cm(sup 2) and require advanced thermal control concepts and technologies to keep their payload within allowable temperature limits. This paper presents background on the need for pumped liquid cooling systems for future micro/nano spacecraft and results from this ongoing experimental investigation.
MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control
NanoSpace 2001: Exploring Interdisciplinary Frontiers, International Conference
2000-11-20
Conference paper
No indication
English
Micro/nano spacecraft thermal control using a MEMS-based pumped liquid cooling system
Tema Archive | 2001
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