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Attitude Determination of the IMS Antarctic Sounding Rockets
https://nipr.repo.nii.ac.jp/records/1137
https://nipr.repo.nii.ac.jp/records/113720615e45-3096-4721-96a1-541e9efdf776
名前 / ファイル | ライセンス | アクション |
---|---|---|
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Item type | 紀要論文(ELS) / Departmental Bulletin Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 1981-03-01 | |||||
タイトル | ||||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
ページ属性 | ||||||
内容記述タイプ | Other | |||||
内容記述 | P(論文) | |||||
著者名(英) |
Tohyama, Fumio
× Tohyama, Fumio× Aoyama, Iwao |
|||||
著者所属(英) | ||||||
en | ||||||
Laboratory of Space Science, Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Laboratory of Space Science, Tokai University | ||||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | During the IMS period (1976-1978), 19 sounding rockets were launched at Syowa Station, Antarctica. 12 rockets of these were S-210 type vehicles and 7 rockets were S-310 type vehicles. Vehicle attitudes have been determinated by use of geomagnetic aspect sensors and other aspect sensors. Most of the S-310 type vehicles took stable flight aspects with the average precession angle about 13 degrees and the period about 192s. In the characteristics of S-210 type vehicle attitudes three kinds were distinguished; the first had aspects of small precession angles and long periods, the second had aspects of large precession angles and short periods, and the third had aspects of intermediate precession angles and periods. The average precession angle of S-210 type vehicles was about 32 degrees and the period was about 72s. | |||||
雑誌書誌ID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00733561 | |||||
書誌情報 |
Memoirs of National Institute of Polar Research. Special issue 巻 18, p. 261-274, 発行日 1981-03 |