dc.contributor.author |
Daimaru, Takuro |
|
dc.contributor.author |
Furst, Benjamin |
|
dc.contributor.author |
Cappucci, Stefano |
|
dc.contributor.author |
Sunada, Eric |
|
dc.contributor.author |
Birur, Gajanana |
|
dc.date.accessioned |
2021-02-25T18:28:45Z |
|
dc.date.available |
2021-02-25T18:28:45Z |
|
dc.date.issued |
2019-07-07 |
|
dc.identifier.citation |
49th International Conference on Environmental Systems (ICES), Boston, Massachusetts, July 7-11, 2019 |
en_US |
dc.identifier.clearanceno |
19-2382 |
|
dc.identifier.uri |
http://hdl.handle.net/2014/51089 |
|
dc.description.abstract |
The Jet Propulsion Laboratory is developing a two-phase mechanically pumped fluid loop (2PMPFL) thermal control system to enable novel mission designs and greater science return for NASA. Pumped two-phase fluid loops have the potential to provide robust and effective thermal control that combine the best aspects of passive two-phase systems (heat pipes) and
mechanically pumped single-phase fluid loops. The current requirements include the development of a system with multiple 1 m2 evaporators, each of which is capable of remaining spatially and temporally isothermal while accommodating heat loads of up to 500 W and local fluxes of up to 5 W/cm2. The goal is to attain this using less than 5 W of power. Such a system would be able to accommodate the next generation of payload and bus
electronics while using minimal resources. |
en_US |
dc.description.sponsorship |
NASA/JPL |
en_US |
dc.language.iso |
en_US |
en_US |
dc.publisher |
Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2019 |
en_US |
dc.title |
Development of an evaporator using porous wick structure for a two-phase mechanically pumped fluid loop |
en_US |
dc.type |
Preprint |
en_US |