Discussion for Orbital Transfer Vehicle Using Electric Propulsion
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- FUNAKI Ikkoh
- Japan Aerospace Exploration Agency
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- NAKANO Masakatsu
- Tokyo Metropolitan College of Industrial Technology
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- KOMURASAKI Kimiya
- The University of Tokyo
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- TAKAO Yoshinori
- Yokohama National University
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- YOKOTA Shigeru
- Tsukuba University
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- CHO Shinatora
- Japan Aerospace Exploration Agency
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- KAWASHIMA Rei
- The University of Tokyo
Bibliographic Information
- Other Title
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- 電気推進を用いた軌道間輸送機に関する議論
Abstract
<p> A panel discussion was held to discuss the technical challenges in orbital transfer vehicle (OTV) development using electric propulsion. Electric propulsion is advantageous in the transportation of SSPS if the solar array panel in the payload can be used in the OTV. Argon is the candidate for the propellant, and the technical issues for the development of high-power argon-propellant thruster are discussed. The collaboration with the ground launch vehicle is indispensable to attain the SSPS, in addition to the cross-field collaboration for the optimization of the OTV. The necessity of technology demonstration missions and technical roadmap is reconfirmed to promote the collaboration among the researchers.</p>
Journal
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- Space Solar Power Systems
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Space Solar Power Systems 5 (0), 1-2, 2020
Space Solar Power Systems Society
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Details 詳細情報について
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- CRID
- 1390002184875696640
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- NII Article ID
- 130007799144
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- ISSN
- 24321060
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- Text Lang
- ja
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- Data Source
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- JaLC
- CiNii Articles
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- Abstract License Flag
- Disallowed