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Thermal Radiation from Plumes of Solid Propellant Rockets
https://jaxa.repo.nii.ac.jp/records/45249
https://jaxa.repo.nii.ac.jp/records/45249fb58607b-0d84-4fc0-a705-373afc9264f3
名前 / ファイル | ライセンス | アクション |
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naltr00990.pdf (3.8 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 | ||||||
言語 | en | |||||
タイトル | Thermal Radiation from Plumes of Solid Propellant Rockets | |||||
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 | 固体ロケットのプルームからの熱放射 | |||||
著者 |
高橋, 守
× 高橋, 守× 泉川, 宗男× 三谷, 徹× 新岡, 嵩× 谷口, 浩文× 兵藤, 幸夫× TAKAHASHI, Mamoru× IZUMIKAWA, Muneo× MITANI, Toru× NIIOKA, Takashi× TANIGUCHI, Hirofumi× HYODO, Yukio |
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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 | ||||||
東北大学 | ||||||
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 | ||||||
Tohoku University | ||||||
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-990 巻 990, p. 33, 発行日 1988-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A simple method for estimating radiative heating by the plumes of solid rockets has been developed. Plume shapes were approximated as bisected conical cylinders with an apex anle. Similarities in the plume shape, the size of plumes and the distribution of radiative power are shown between subscale motors and the SRB of space shuttles. All radiation is assumed to be emitted from the surface of the cylinder. The effects of the interior of the plumes is confined to the emissivity of the surface. The emissivity of the plume can be related to its optical thickness, and the optical thickness can be estimated from the number density and the diameter of particles in the plume. Dependence of radiative heating on motor size and flight altitude can be explained in terms of similarities in plume radiation. | |||||
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: NALTR0990000 | |||||
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-990 |