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固体ロケット残留推力の実験
https://jaxa.repo.nii.ac.jp/records/45058
https://jaxa.repo.nii.ac.jp/records/450580d814510-4810-410c-8d83-f3d8ad8c038d
名前 / ファイル | ライセンス | アクション |
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naltr00800.pdf (2.8 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 | 固体ロケット残留推力の実験 | |||||
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 | Experiments on Residual Thrust and Prediction for Upper-Stage Solid Propellant Rockets. | |||||
著者 |
三谷, 徹
× 三谷, 徹× 高橋, 守× 新岡, 嵩× 日下, 和夫× 熊谷, 達夫× 只野, 真× 須藤, 孝幸× 宮島, 博× 斉藤, 紀男× 丹尾, 新治× 江口, 昭裕× MITANI, Toru× TAKAHASHI, Mamoru× NIIOKA, Takashi× KUSAKA, Kazuo× KUMAGAI, Tatsuo× TADANO, Makoto× SUDO, Takayuki× MIYAJIMA, Hiroshi× SAITO, Norio× NIO, Shinji× EGUCHI, Akihiro |
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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 | ||||||
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 | ||||||
宇宙開発事業団 | ||||||
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 | ||||||
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) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
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-800 巻 800, p. 18, 発行日 1984-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 150mm径円筒状及び8光芒固体ロケットモータと380mm径球型ロケットモータの燃焼実験を行ない,燃焼終了後に発生する微少な残留内圧を測定した。低圧室内で測定された残留内圧は,ノズルでのガス流れを考慮して,真空におけるモータチャンバ圧に補正し,残留推力のメカニズムを詳細に検討した。これらの小さなロケットモータの実験結果に理論的検討から得られた残留推力の寸法効果を考慮して,130mm径モータ(HI-3段モータ相当)の残留推力の大きさを予測した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Subscale rocket motors of 150mm(cylindrical) in dia.and 380mm(spherical) in dia.were tested to investigate the small residual thrust of solid propellant rockets. The residual chamber pressure was measured by using pressure gages with full ranges of 2.5 and 5 psia(0.334 and 0.668 kPa)in a high altitude simulation facility. The motor chamber pressure measured in the low pressure cell(about 3.34 kPa) was corrected to that of a vacuum. The mechanism of the residual thrust is discussed in this paper. From the scale effect of the residual thrust of a large-scale motor corresponding to the HI-3rd stage motor is predicted from the results of these experiments. | |||||
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: NALTR0800000 | |||||
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-800 |