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Prediction of the Maximum Force Acting on the Load Cell and Thrust Transient during Rocket Motor Firing Tests
https://jaxa.repo.nii.ac.jp/records/44893
https://jaxa.repo.nii.ac.jp/records/448934e5b8d8f-18a2-4697-8208-b2ba22cf17bd
名前 / ファイル | ライセンス | アクション |
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naltr00638.pdf (1.3 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 | ||||||
言語 | en | |||||
タイトル | Prediction of the Maximum Force Acting on the Load Cell and Thrust Transient during Rocket Motor Firing Tests | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | ロケット地上燃焼実験時のロードセル最大荷重と推力立上り特性の推定 | |||||
著者 |
工藤, 賢司
× 工藤, 賢司× 村上, 淳郎× 小室, 智幸× 石井, 進一× 梶原, 堅一× KUDO, Kenji× MURAKAMI, Atsuo× KOMURO, Tomoyuki× ISHII, Shin-ichi× KAJIWARA, Kenichi |
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著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
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報告 en : Technical Report of National Aerospace Laboratory TR-638 巻 638, p. 18, 発行日 1980-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An impulse test for a thrust stand was conducted and a mathematical model to simulate the main thrust measurement system was presented in order to predict the maximum force acting on the load cell and thrust transient characteristics during rocket motor firing tests. An approximating expression for the maximum force acting on the load cell was obtained from the mathematical model and its results agreed well with experimental values. The prediction of the thrust transient was made by using a mathematical model and four alternative methods, and each of their features and problems was described. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0638000 | |||||
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 TR-638 |