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Author | Hadj-Nacer, Mustafa | |
Author | Greiner, Miles | |
Author | Kim, Kwang | |
Author | Cooper, Clay | |
Author | Plaggemeyer, Ted | |
Date Accessioned | 2019-09-25T17:24:34Z | |
Date Available | 2019-09-25T17:24:34Z | |
Date of Issue | 2016-04 | |
Identifier (URI) | http://hdl.handle.net/11714/6298 | |
Description | 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. | |
Sponsorship | NASA EPSCoR | en_US |
Language | en_US | en_US |
Title | Advanced Transport Technologies for NASA Thermal Management/Control Systems | en_US |
Type | Technical Report | en_US |