月探査利用の研究:月軟着陸実験機に向けて

Material type: 文書・図像類

Author: 松本, 甲太郎ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

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Note (General)：: Lunar Exploration and Utilization become the major trend in the world space development, in these couple of years. As the follow-on project of SELENE,...

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Material Type: 文書・図像類
Title: 月探査利用の研究:月軟着陸実験機に向けて
Author/Editor: 松本, 甲太郎
佐々, 修一
若林, 幸子
星野, 健
松本, 康司
片山, 保宏
二宮, 哲次郎
濱田, 吉郎
四宮, 康雄
Matsumoto, Kotaro
Sasa, Shuichi
Wakabayashi, Sachiko
Hoshino, Takeshi
Matsumoto, Koji
Katayama, Yasuhiro
Ninomiya, Tetsujiro
Hamada, Yoshiro
Shinomiya, Yasuo
Author Heading: 松本, 甲太郎
佐々, 修一
若林, 幸子
星野, 健
松本, 康司
片山, 保宏
二宮, 哲次郎
濱田, 吉郎
四宮, 康雄
Matsumoto, Kotaro
Sasa, Shuichi
Wakabayashi, Sachiko
Hoshino, Takeshi
Matsumoto, Koji
Katayama, Yasuhiro
Ninomiya, Tetsujiro
Hamada, Yoshiro
Shinomiya, Yasuo
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-20
Publication Date (W3CDTF): 2006-01-20
Alternative Title: Study on lunar exploration and utilization: For the lunar soft landing experiment
Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:先行研究等 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Pioneering Research
No. or year of volume/issue: JAXA-SP-05-011
Volume: JAXA-SP-05-011
Pages: 61-66
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 月探査
月軟着陸
SELENE-B
画像処理
障害物検知
レゴリス
月探査ローバ
極低温
真空チャンバー
lunar exploration
lunar soft landing
image processing
obstacle detection
regolith
moon rover
cryogenic temperature
vacuum chamber
Target Audience: 一般
Note (General): Lunar Exploration and Utilization become the major trend in the world space development, in these couple of years. As the follow-on project of SELENE, we had studied the first Japanese moon lander as SELENE-B from 2001. In SELENE-B, the exploration of the vicinity of a central peak of a crater, and the sure obstacle avoidance and safe landing were the major mission objectives. Corresponding to the new world trend for international Lunar exploration, we have expanded our mission purpose and research targets from lunar science to lunar exploration and utilization. For these extended mission purposes, severe technological requirements should still be solved for the implementation of these new missions. The lunar lander has to detect obstacles, such as crater or rocks, and land at the safe area. After the landing, the investigation will be done on the very rocky and rough terrain. The lander system will be requested to survive against the very low temperature (around 80 K) during the Lunar night. This paper reports the current studies on these technological subjects for the future lunar base.
資料番号: AA0049057015
レポート番号: JAXA-SP-05-011
Access Restrictions: 限定公開
Periodical Title (NCID): AA11984031
https://ci.nii.ac.jp/ncid/AA11984031
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ