NASA NTRS · 20060031280
MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control
Abstract
The objective is to develop MEMS based pumped liquid cooling system for removing over 20 W/cm squared from high power density microelectronics and science payloads considered for future micro/nano sciencecraft.
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Birur, G. C., Shakkottai, P., Sur, T. W. 2001-03-13. MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control. https://ntrs.nasa.gov/citations/20060031280
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