| タイトル | Element Technologies for Trajectory Design for Lunar/Planetary Exploration |
| 著者（日） | 寺田, 博; 松岡, 正敏; 田中, 貴美恵; 鵜飼, 千亜妃 |
| 著者（英） | Terada, Hiroshi; Matsuoka, Masatoshi; Tanaka, Kimie; Ukai, Chiaki |
| 著者所属（日） | NEC航空宇宙システム; NEC航空宇宙システム; NEC航空宇宙システム; NEC航空宇宙システム |
| 著者所属（英） | NEC Aerospace Systems; NEC Aerospace Systems; NEC Aerospace Systems; NEC Aerospace Systems |
| 発行日 | 2011-04-25 |
| 発行機関など | 日本電気
NEC |
| 刊行物名 | NEC Technical Journal |
| 巻 | 6 |
| 号 | 1 |
| 開始ページ | 132 |
| 終了ページ | 136 |
| 刊行年月日 | 2011-04-25 |
| 言語 | eng |
| 抄録 | Trajectory design for lunar/planetary probes requires technologies different from those required by Earth-orbiting satellites. NEC has long been in charge of trajectory design for many lunar and planetary probes in cooperation with the Japan Aerospace Exploration Agency (JAXA) and its predecessor organization. This paper gives an outline of the main technology elements involved and the trajectory design characteristics of various projects based on them. |
| キーワード | trajectory design; lunar/planetary probe; swing-by; launch window; electrical propulsion; planetary exploration; lunar exploration |
| 資料種別 | Journal Article |
| ISSN | 1880-5884 |
| NCID | AN00330367 |
| SHI-NO | AA0065008023 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/17666 |
