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Study of the PBE Cycle 100kN LH2/LO2 Rocket Engine
https://jaxa.repo.nii.ac.jp/records/45224
https://jaxa.repo.nii.ac.jp/records/45224f816f785-24db-4427-a6e3-71da0b046c73
名前 / ファイル | ライセンス | アクション |
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naltr00965.pdf (1.7 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 | Study of the PBE Cycle 100kN LH2/LO2 Rocket Engine | |||||
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 | PBEサイクル100kN級のLH2/LO2ロケットエンジンの検討 | |||||
著者 |
苅田, 丈士
× 苅田, 丈士× 若松, 義男× 橋本, 亮平× 冠, 昭夫× KANDA, Takeshi× WAKAMATSU, Yoshio× HASHIMOTO, Ryohei× KANMURI, Akio |
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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 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
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 | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
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-965 巻 965, p. 20, 発行日 1988-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We have previously reported that the PBE (Partial Bleed Expander) cycle LH2/LO2 engine has good performance at a 10kN-thrust. In this report, we discuss the PBE cycle LH2/LO2 engine and other low-temperature-cycle engines at a 100kN-thrust. The PBE cycle 100kN engine has the same engine performance as that of the GG (Gas generater) cycle engine. Among the engine whose thrust chambers are regeneratively cooled, the PBE cycle 100kN engine has the best performance; start transient simulation analysis showed that the PBE cycle engine can start without trouble. It is not suitable that both the nozzle skirt and the thrust chamber of the PBE cycle 100kN engine be regeneratively cooled. | |||||
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: NALTR0965000 | |||||
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-965 |