長パルス1次レーダーによるUSERS REVカプセルの追跡

• 資料種別: 規格・テクニカルリポート類
• タイトル: 長パルス1次レーダーによるUSERS REVカプセルの追跡
• 著者・編者: 鎌田, 幸男; 川原, 康介; 佐川, 一美; 石井, 信明; 前田, 行雄; 井上, 浩三郎; 安部, 隆士; 若林, 昭; 伊地智, 幸一; Kamata, Yukio; Kawahara, Kosuke; Sagawa, Kazumi; Ishii, Nobuaki; Maeda, Yukio; Inoue, Kozaburo; Abe, Takashi; Wakabayashi, Akira; Ijichi, Koichi
• 著者標目: 鎌田, 幸男; 川原, 康介; 佐川, 一美; 石井, 信明; 前田, 行雄; 井上, 浩三郎; 安部, 隆士; 若林, 昭; 伊地智, 幸一; Kamata, Yukio; Kawahara, Kosuke; Sagawa, Kazumi; Ishii, Nobuaki; Maeda, Yukio; Inoue, Kozaburo; Abe, Takashi; Wakabayashi, Akira; Ijichi, Koichi
• 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）: 2005-03-31
• 並列タイトル等: Orbit tracking of USERS Recovery Vehicle (REV) with a high performance long pulse primary radar
• タイトル（掲載誌）: 宇宙航空研究開発機構研究開発報告: USERS REVカプセルの開発研究および飛行後解析 = JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis
• 巻号年月日等（掲載誌）: JAXA-RR-04-045
• 掲載巻: JAXA-RR-04-045
• 掲載ページ: 105-111
• ISSN（掲載誌）: ISSN : 1349-1113
• 本文の言語コード: jpn
• 件名標目: USERSミッション; 宇宙機再突入; リエントリモジュール; 長パルス1次レーダ; 回収機; 再突入飛跡; 追尾アンテナ; USERS mission; spacecraft reentry; reentry module; long pulse primary radar; recovery vehicle; reentry trajectory; tracking antenna
• 対象利用者: 一般
• 一般注記: 出版タイプ： NA; After 8.5 month-experiments in orbit, the Recovery Vehicle (REV) of the USERS satellite was reentered into the atmosphere and successfully retrieved on the sea in May 30th, 2003. During the atmospheric flight, the trajectory of the vehicle was tracked with the new precision radar system at Kagoshima Space Center, Uchinoura, Kagoshima. Since, the vehicle has no active tracking instrument such as transponder, the primary radar should be utilized so as to detect the object. However, the usual primary radar system is insufficient to track the tiny vehicle. Thus, a high performance long-pulse primary radar, which had capability of recognizing the 1 sq m object at the distant of approximately 2,000 km range, was applied to the tracking operation. Initially, the radar caught the reentry vehicle in the previously predicted direction. However, the radar lost the tracking data, intermediately. In this paper, the operation sequence of the reentry tracking is briefly introduced. Then, the tracking result is summarized with the estimation of the impact point by the off-line computation.; 資料番号: AA0048710007; レポート番号: JAXA-RR-04-045
• 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