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固体ロケットの比推力測定の標準化
https://jaxa.repo.nii.ac.jp/records/43787
https://jaxa.repo.nii.ac.jp/records/437877912a0b0-6e7c-46f3-88d7-71736eb7d2c6
名前 / ファイル | ライセンス | アクション |
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naltm00203.pdf (3.4 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 | 固体ロケットの比推力測定の標準化 | |||||
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 | Standard Ballistic Test Evaluation System for Solid Rocket Propellants | |||||
著者 |
五代, 富文
× 五代, 富文× 岡部, 裕二郎× 清水, 昭紀× 伊藤, 克弥× 西村, 久男× GODAI, Tomifumi× OKABE, Yujiro× SHIMIZU, Shoki× ITO, Katsuya× NISHIMURA, Hisao |
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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宇宙研究グループ | ||||||
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 203, p. 26, 発行日 1971-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An accurate and standard specific impulse measurement system with an overall error not exceeding 0.1% for solid rocket propellants is described. After investigating a con- ventional specific impulse measurement system existing at the National Aerospace Laboratory, some new design concepts, consideration of ballistic evaluation of a solid rocket motor, an accurate thrust stand, and electronic equipment and environmental conditions are discussed. The results of system tests, static calibration and motor firing tests are also described. | |||||
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: NALTM0203000 | |||||
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-203 |