Advances in Spacecraft Brine Water Recovery: Development of a Radial Vaned Capillary Drying Tray
| dc.creator | Callahan, Michael R. | |
| dc.creator | Sargusingh, Miriam J. | |
| dc.creator | Pickering, Karen D. | |
| dc.creator | Weislogel, Mark M. | |
| dc.date.accessioned | 2014-10-20T20:03:35Z | |
| dc.date.available | 2014-10-20T20:03:35Z | |
| dc.date.issued | 2014-07-13 | |
| dc.description | The 44th International Conference on Environmental Systems was held in Tuscon, Arizona, USA on 13 July 2014 through 17 July 2014. | |
| dc.description | Michael R. Callahan, NASA Johnson Space Center, USA | |
| dc.description | Miriam J. Sargusingh, NASA Johnson Space Center, USA | |
| dc.description | Karen D. Pickering, NASA Johnson Space Center, USA | |
| dc.description | Mark M. Weislogel, Portland State University, USA | |
| dc.description.abstract | Technology improvements in the recovery of water from brine are critical to establishing closed-loop water recovery systems, enabling long—duration missions, and achieving a sustained human presence in space. A genre of ‘in-place drying’ brine water recovery concepts, collectively referred to herein as Brine Residual In-Containment, are under development. These brine water recovery concepts aim to increase the overall robustness and reliability of the brine recovery process by performing drying inside the container used for final disposal of the solid residual waste. Implementation of in-place drying techniques have been demonstrated for applications where gravity is present and phase separation occurs naturally by buoyancy—induced effects. In this work, a microgravity—compatible analogue of the gravity-driven phase separation process is considered by exploiting capillarity in the form of surface wetting, surface tension, and container geometry. The proposed design consists of a series of planar radial vanes aligned about a central slotted core. Preliminary testing of the fundamental geometry in a reduced gravity environment has shown the device to spontaneously fill and saturate rapidly, thereby creating a free surface from which evaporation and phase separation can occur similar to a terrestrial-like ‘cylindrical pool’ of fluid. Mathematical modeling and analysis of the design suggest predictable rates of filling and stability of fluid containment as a function of relevant system dimensions; e.g., number of vanes, vane length, width, and thickness. A description of the proposed capillary design solution is presented along with preliminary results from testing, modeling, and analysis of the system. | en_US |
| dc.format.mimetype | application/pdf | |
| dc.identifier.isbn | 978-0-692-38220-2 | |
| dc.identifier.other | ICES-2014-260 | |
| dc.identifier.uri | http://hdl.handle.net/2346/59658 | |
| dc.language.iso | eng | en_US |
| dc.publisher | 44th International Conference on Environmental Systems | en_US |
| dc.title | Advances in Spacecraft Brine Water Recovery: Development of a Radial Vaned Capillary Drying Tray | en_US |
| dc.type | Presentation | en_US |