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安定板を有する固体ロケットの操舵要求軽減法
https://jaxa.repo.nii.ac.jp/records/43799
https://jaxa.repo.nii.ac.jp/records/43799a165a234-83f0-43c7-af7d-1f8793fccc29
名前 / ファイル | ライセンス | アクション |
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naltm00216.pdf (1.5 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 安定板を有する固体ロケットの操舵要求軽減法 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | An Estimation of Deflection Requirements of An Aero-Stable Solid Propellant Rocket Vehicle | |||||
著者 |
大石, 晃
× 大石, 晃× 山中, 龍夫× 冠, 昭夫× OOISHI, Akira× YAMANAKA, Tatsuo× KAMMURI, Akio |
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著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 216, p. 36, 発行日 1972-02 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, are estimated the peak deflection angles and the total injectants required to control an aero-stable solid propellant rocket vehicle (the 1st stage) by SITVC (secondary injection thrust vector control) system. It is desirable to minimize those values under the given constraints; to minimize the aerodynamic load on the body, to minimize the flow rate capacity of the injection valves and to minimize the capacity of the injectants feed system. In order to realize the mini-mum deflection angles, the load relief auto-pilot method is used. A non-gravity-turn nominal trajectory is presented to reduce the effects of wind disturbance. The results of the computer simulation are discussed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0216000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-216 |