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Advanced Transport Technologies for NASA Thermal Management/Control Systems
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The objective of this project is to develop technologies that can be used to design mechanicallypumped two-phase cooling loop in microgravity for NASA Space systems. Specifically, design a system with a ~1-m2 -flat coolant plate whose temperature can be controlled to better than 1 K isothermality with discrete and time-varying heat loads of ~5W/cm2.