| タイトル | 超小型衛星HIT-SATの熱・構造設計 |
| その他のタイトル | Thermal and structural design of subminiature satellite HIT-SAT |
| 著者（日） | 佐鳥 新; 戸谷 剛; 榊原 隆浩; 安中 俊彦; 植松 努; 石村 康生; 杉本 康一郎; 松島 幸太; 三橋 龍一; 西舘 純 |
| 著者（英） | Satori, Shin; Totani, Tsuyoshi; Sakakibara, Takahiro; Yasunaka, Toshihiko; Uematsu, Tsutomu; Ishimura, Kosei; Sugimoto, Koichiro; Matsushima, Kota; Mitsuhashi, Ryuichi; Nishidate, Jun |
| 著者所属（日） | 北海道工業大学; 北海道大学; 北海道大学; 植松電機; 植松電機; 北海道大学; 北海道大学; 北海道大学; 北海道工業大学; 北海道工業大学 大学院工学研究科 |
| 著者所属（英） | Hokkaido Institute of Technology; Hokkaido University; Hokkaido University; Uematsu Electric Co. Ltd.; Uematsu Electric Co. Ltd.; Hokkaido University; Hokkaido University; Hokkaido University; Hokkaido Institute of Technology; Hokkaido Institute of Technology Graduate School of Engineering |
| 発行日 | 2007-03 |
| 刊行物名 | 北海道工業大学研究紀要
Memoirs of the Hokkaido Institute of Technology |
| 号 | 35 |
| 開始ページ | 105 |
| 終了ページ | 111 |
| 刊行年月日 | 2007-03 |
| 言語 | jpn |
| 抄録 | HIT-SAT (Hokkaido Institute of Technology Satellite) has been designed and developed in order to examine functions of the bus system. It was launched by M-V-7 into a sun-synchronous orbit of the altitude of 279-660 km and the inclination of 98.32 deg. The volume and weight of HIT-SAT are about 12 x 13 x 12 cu cm and 2.7 kg, respectively. HIT-SAT has a flame-panel structure that consists of six panels, four columns and two shelves made of the aluminum alloy that has a high conductivity. The load pass at the launch is their panels and columns. The passive thermal control is adopted. Random vibration tests and impact tests were carried out. It has been concluded that HIT-SAT is unbreakable by the vibration and the impact at launch. Thermal analysis is conducted using Thermal Desktop/SINDA/FLUINT. It has been clear that HIT-SAT works in orbit. |
| キーワード | subminiature satellite; small scientific satellite; satellite design; passive thermal control; piggyback system; satellite attitude control; structural vibration; vibration test; impact test; HIT-SAT; 超小型衛星; 小型科学衛星; 衛星設計; 受動的熱制御; ピギーバックシステム; 衛星姿勢制御; 構造振動; 振動試験; 衝撃試験; HIT-SAT |
| 資料種別 | Technical Report |
| ISSN | 0385-0862 |
| SHI-NO | AA0063211005 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/51173 |
