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

• Material Type: 文書・図像類
• Title: Lunar Imaging Camera (LIC): Pre-flight tests and operation plan
• Author/Editor: 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
• Author Heading: 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
• Publication, Distribution, etc.: 宇宙航空研究開発機構
• Publication Date: 2005-03-31
• Publication Date (W3CDTF): 2005-03-31
• Alternative Title: 月撮像カメラ(LIC):飛行前試験及び運用計画
• Periodical title: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report
• No. or year of volume/issue: JAXA-RR-04-046E
• Volume: JAXA-RR-04-046E
• ISSN (Periodical Title): ISSN : 1349-1113
• Text Language Code: eng
• Subject Heading: 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
• Target Audience: 一般
• Note (General): 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
• Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2315&item_no=1&attribute_id=31&file_no=1
• Access Restrictions: 限定公開
• 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