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二次噴射による固体ロケットの推力方向制御の研究
https://jaxa.repo.nii.ac.jp/records/44657
https://jaxa.repo.nii.ac.jp/records/4465775383935-e01e-4a4d-81f8-7455ba80ad9d
名前 / ファイル | ライセンス | アクション |
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naltr00409.pdf (958.0 kB)
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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 | 二次噴射による固体ロケットの推力方向制御の研究 | |||||
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 | Thrust Vector Control by Secondary Injection into Rocket Nozzles | |||||
著者 |
石井, 進一
× 石井, 進一× 鎮西, 信夫× 工藤, 賢司× 山田, 晃× ISHII, Shinichi× CHINZEI, NOBUO× KUDO, Kenji× YAMADA, AKIRA |
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著者所属 | ||||||
角田支所 | ||||||
著者所属 | ||||||
角田支所 | ||||||
著者所属 | ||||||
角田支所 | ||||||
著者所属 | ||||||
角田支所 | ||||||
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) | ||||||
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-409 巻 409, p. 13, 発行日 1975-02 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents an experimental result of secondary injection thrust vector control and an approximate analysis of estimating the control forces produced by liquid injection. The experiment was conducted with the solid rocket motors of about 400kg thrust. The control forces produced by the secondary injection were measured by a four-component test stand. The nozzle was conical, of which expansion ratio was 1:8.1. Fluids of various kinds were used as the injectants, i.e.hydrogen peroxide(90%wt), decomposed gas of hydrogen peroxide(90%wt), Freon 114B2 and strontium perchlorate(70%wt). The effects of injection location and the injectant flow rate on the produced control forces have been well illustrated by the experiment. An approximate analytical model to predict the disturbance induced by secondary liquid injection has been presented also. The estimated control forces based on the flow model are compared with the experimental results for cases of hydrogen peroxide and Freon 114B2. | |||||
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: NALTR0409000 | |||||
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-409 |