Lunar Imaging Camera (LIC): Pre-flight tests and operation plan

• 資料種別: 規格・テクニカルリポート類
• タイトル: Lunar Imaging Camera (LIC): Pre-flight tests and operation plan
• 著者・編者: 中村, 昭子; 白石, 浩章; 本田, 理恵; 飯島, 祐一; 橋本, 樹明; 二宮, 敬虔; 横田, 康弘; 白尾, 元理; 高田, 淑子; 山路, 敦; Nakamura, Akiko M.; Shiraishi, Hiroaki; Honda, Rie; Iijima, Yuichi; Hashimoto, Tatsuaki; Ninomiya, Keiken; Yokota, Yasuhiro; Shirao, Motomaro; Takata, Toshiko; Yamaji, Atsushi
• 著者標目: Nakamura, Akiko M.; Shiraishi, Hiroaki; Honda, Rie; Iijima, Yuichi; Hashimoto, Tatsuaki; Ninomiya, Keiken; Yokota, Yasuhiro; Shirao, Motomaro; Takata, Toshiko; Yamaji, Atsushi
• 出版事項: 宇宙航空研究開発機構
• 出版年月日等: 2005-03-31
• 出版年（W3CDTF）: 2005
• 並列タイトル等: 月撮像カメラ(LIC):飛行前試験及び運用計画
• タイトル（掲載誌）: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report
• 巻号年月日等（掲載誌）: JAXA-RR-04-046E
• 掲載巻: JAXA-RR-04-046E
• ISSN（掲載誌）: ISSN : 1349-1113
• 件名標目: 月探査; 月撮像カメラ; CCDカメラ; 月のクレータ; レゴリス; 光学装置; スペクトル感度; 飛行前試験; lunar exploration; lunar imaging camera; CCD camera; lunar crater; regolith; optical equipment; spectral sensitivity; preflight test
• 対象利用者: 一般
• 一般注記: 出版タイプ： NA; Lunar Imaging Camera (LIC) is a small, compact and lightweight monochromatic imager designed and developed for LUNAR-A, Japanese lunar mission. The scientific objectives of the camera address impact cratering, tectonic processes, volcanic features, and optical properties of the regolith surface. The image sensor is a linear CCD and is aligned with the spin axis of the spacecraft, which orbits the Moon at altitudes of 200 - 300 km. The two-dimensional image is taken using the spin motion of the spacecraft. The total Field Of View (FOV) of the camera is 360 deg (around the spin axis) x 14.6 deg (along the CCD-array). LIC obtains an image in one spin. The angular resolution of the camera is about 20 arcsec/pixel at a spin rate of 3 rpm. The spatial resolution is about 25 m/pixels at the surface when the altitude is 250 km. The spin axis of the LUNAR-A approximately points toward the Sun, therefore, LIC can take images of the lunar surface with highly oblique illumination conditions near the terminator. A series of pre-flight tests of LIC was performed. In those tests, the hardware performance and the functions of LIC were verified and the data for radiometric and geometric corrections were obtained. This paper outlines the scientific objective, characteristics of LIC, the procedure and the results of the pre-flight tests and the operation plan of LIC.; 資料番号: AA0048703000; レポート番号: JAXA-RR-04-046E
• 掲載誌（NCID）: AA1192675X; https://ci.nii.ac.jp/ncid/AA1192675X
• 連携機関・データベース: 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
• 提供元機関・データベース: 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