may not work without it.
If you have any problems related to the accessibility of any content (or if you want to request that a specific publication be accessible), please contact (email@example.com). We will work to respond to each request in as timely a manner as possible.
Advanced Transport Technologies for NASA Thermal Management/Control Systems
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.