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- YOSHIKAWA Kent
- Japan Aerospace Exploration Agency
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- OTSUKI Masatsugu
- Japan Aerospace Exploration Agency
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- YOSHIMITSU Tetsuo
- Japan Aerospace Exploration Agency
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- MAEDA Takao
- Chuo University
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- KUNII Yasuharu
- Chuo University
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- HIRANO Daichi
- Japan Aerospace Exploration Agency
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- SUTOH Masataku
- Japan Aerospace Exploration Agency
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- Sawada Hirotaka
- Japan Aerospace Exploration Agency
Bibliographic Information
- Other Title
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- 超小型月面探査ローバの開発
Description
This paper presents the current development status of the optional payload named Lunar Excursion Vehicle (LEV) for the Japanese future Lunar landing mission SLIM. The deployable exploration system LEV is released from the lander at the few meters above the Lunar surface after the lander’s terminal deceleration is finished. LEV consists of two probes that will move and observe around the landing site autonomously. They also help acquire the evidence of SLIM landing by taking pictures of the final status of the lander.
Journal
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- The Proceedings of the Symposium on the Motion and Vibration Control
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The Proceedings of the Symposium on the Motion and Vibration Control 2019.16 (0), A103-, 2019
The Japan Society of Mechanical Engineers
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Details 詳細情報について
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- CRID
- 1390285300169731200
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- NII Article ID
- 130007864817
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- ISSN
- 24243000
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed