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NASACompany
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.NASA EPSCo
The miniaturization of cryogenic components plays a significant role in the never ending quest for ...
The increasing thermal demands for spacecraft require the development of new technologies. To effici...
This paper presents an advanced miniature heat transport system for thermal control of small spacecr...
Thermal and mechanical technologies are an important part of the Deep Space Systems Technology (DSST...
PGBA, a 0.08m2 / 27 liter spaceflight plant chamber payload employs two temperature-controlled liqui...
A wide range of fi~ture space missions are expected to utilize the technologies and the architecture...
A description of recent and planned thermal control technology developments at the Johnson Space Cen...
Initial studies have indicated that in comparison to an all liquid single phase system, a two-phase ...
Future large spacecraft, such as the Earth Observing System (EOS) platforms, will require a signific...
Abstract- NASA’s New Millennium Program funded an effort to develop a system cooling technology, whi...
Technology development is inevitably a dynamic process in search of an elusive goal. It is never tru...
Realization of Responsive Space (RS) program goals requires further progress in reducing the time re...
Abstract: This paper presents an advanced miniature heat transport system for thermal control of sma...
Technology development is inevitably a dynamic process in search of an elusive goal. It is never tru...
Small spacecraft have typically relied on thermal control systems in which waste heat is simply cond...
The miniaturization of cryogenic components plays a significant role in the never ending quest for ...
The increasing thermal demands for spacecraft require the development of new technologies. To effici...
This paper presents an advanced miniature heat transport system for thermal control of small spacecr...
Thermal and mechanical technologies are an important part of the Deep Space Systems Technology (DSST...
PGBA, a 0.08m2 / 27 liter spaceflight plant chamber payload employs two temperature-controlled liqui...
A wide range of fi~ture space missions are expected to utilize the technologies and the architecture...
A description of recent and planned thermal control technology developments at the Johnson Space Cen...
Initial studies have indicated that in comparison to an all liquid single phase system, a two-phase ...
Future large spacecraft, such as the Earth Observing System (EOS) platforms, will require a signific...
Abstract- NASA’s New Millennium Program funded an effort to develop a system cooling technology, whi...
Technology development is inevitably a dynamic process in search of an elusive goal. It is never tru...
Realization of Responsive Space (RS) program goals requires further progress in reducing the time re...
Abstract: This paper presents an advanced miniature heat transport system for thermal control of sma...
Technology development is inevitably a dynamic process in search of an elusive goal. It is never tru...
Small spacecraft have typically relied on thermal control systems in which waste heat is simply cond...
The miniaturization of cryogenic components plays a significant role in the never ending quest for ...
The increasing thermal demands for spacecraft require the development of new technologies. To effici...
This paper presents an advanced miniature heat transport system for thermal control of small spacecr...
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