Abstract
Because the Martian atmosphere is composed mainly of , electrochemical conversion of to is one of the most efficient methods of extracting oxygen, which is indispensable for astronauts to breathe and can be used as an oxidant for rocket engines. In order to realize a reliable oxygen production system, a large amount of gas must be accumulated and compressed in an electrolytic conversion system. However, dust present in the Martian atmosphere because of dust storms could damage the oxygen conversion system or cause it to malfunction. Thus, a dust removal system is necessary before gas can be introduced into the system. To this end, an electrostatic precipitator suitable for use in the low-pressure Martian atmosphere has been developed. First, a precipitator consisting of a wire and parallel-plate electrodes was constructed. In a preliminary study, the efficiency of dust removal was 75%–80% without corona discharge, and almost no dust was collected at the corona discharge region in the low-pressure (700 Pa) atmosphere that simulated the Martian atmosphere. In this case, dust was collected on the surface of the wire electrode, contrary to the case for a pressure of (1 atm). The mechanism of these phenomena was investigated by direct observation and numerical calculation of particle motion in the precipitator. It was clarified that the low charge density of particles in the low-pressure atmosphere caused a relatively large dielectrophoresis force in comparison with the Coulomb force, and the particles were attracted to the wire electrode, i.e., the dielectrophoresis forces dominate in the low-pressure regime, whereas Coulomb forces dominate in the high-pressure regime. Poor performance in the low-pressure atmosphere was caused by the low charge density and low electrostatic field owing to the low limited voltage. Although the performance deteriorated rapidly in the low-pressure atmosphere because of the deposition of dust on the fine wire electrode, it was easy to vibrate the wire electrode and remove dust on the wire.
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Acknowledgments
The authors would like to express their gratitude to Shuta Inari, Tomoki Kobayakawa, Yuki Ogino, Ryotaro Sawai, Cheng Kedong, and Yuki Matsumoto of Waseda University for their support in conducting the experiment. A part of this work was supported by JSPS KAKENHI Grant No. 17K06276 and the Iwatani Naoji Foundation.
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©2019 American Society of Civil Engineers.
History
Received: Mar 7, 2018
Accepted: Sep 26, 2018
Published online: Jan 25, 2019
Published in print: May 1, 2019
Discussion open until: Jun 25, 2019
ASCE Technical Topics:
- [Inorganic compounds]
- Aerospace engineering
- Analysis (by type)
- Astronomy
- Carbon compounds
- Carbon dioxide
- Chemicals
- Chemistry
- Climates
- Dust
- Electrokinetics
- Engineering fundamentals
- Engineering materials (by type)
- Environmental engineering
- Mars
- Materials engineering
- Meteorology
- Numerical analysis
- Organic compounds
- Particles
- Planets
- Pollutants
- Precipitation
- System reliability
- Systems engineering
- Systems management
- Waste management
Notes
A part of this paper was presented at the 47th International Conference on Environmental Systems (ICES 2017), July 17, 2017, in Charleston, South Carolina (Kawamoto et al. 2017).
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