Technical Papers
May 12, 2018

Electrostatic Sampling and Transport of Ice for In-Situ Resource Utilization

Publication: Journal of Aerospace Engineering
Volume 31, Issue 4

Abstract

It has been discovered that water (ice) exists at the polar regions of the Moon and Mars, and it is expected that water would be used to maintain life support for astronauts and to provide a raw material of hydrogen and oxygen. Because it is necessary to mine, sample, and transport water ice for in-situ water utilization, electrostatic sampling and transport systems for crushed water ice have been developed. A high voltage is applied between parallel screen electrodes of the sampling device. It was demonstrated that crushed ice particles, as well as regolith particles, can be captured successfully by the screen electrodes as a result of the electrostatic force if the lower screen electrode is placed in contact with the surface of the ice bulk. Ion-exchanged water ice, tap-water ice, CuSO4-doped water ice, and ice mixed with lunar regolith simulant were captured. Captured ice particles are transported by the electrostatic transport system that uses electrostatic traveling waves. The conveyer consists of parallel electrodes printed on a plastic substrate. A four-phase rectangular voltage is applied to the electrodes to transport particles on the conveyer. It was demonstrated that crushed ice particles mixed with lunar regolith simulant, as well as regolith particles and liquid water droplets, are transported successfully by this system.

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Acknowledgments

The author would like to express his gratitude to Sota Fukuyama and Shuhei Watanabe (Waseda University) for their support in conducting the experiment. A part of this work was supported by JSPS KAKENHI Grant No. 17K06276.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 31Issue 4July 2018

History

Received: Aug 10, 2017
Accepted: Jan 16, 2018
Published online: May 12, 2018
Published in print: Jul 1, 2018
Discussion open until: Oct 12, 2018

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Authors

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Hiroyuki Kawamoto [email protected]
Professor, Dept. of Applied Mechanics and Aerospace Engineering, Waseda Univ., 3-4-1, Okubo, Shinjuku, Tokyo 169-8555, Japan (corresponding author). Email: [email protected]
Naonori Yoshida [email protected]
Dept. of Applied Mechanics and Aerospace Engineering, Waseda Univ., 3-4-1, Okubo, Shinjuku, Tokyo 169-8555, Japan. Email: [email protected]

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