Study of the PBE Cycle 100kN LH2/LO2 Rocket Engine

Material type: 文書・図像類

Author: 苅田, 丈士ほか

Publisher: 航空宇宙技術研究所

Publication date: 1988-03

Material Format: Digital

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Note (General)：: 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 discu...

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Material Type: 文書・図像類
Title: Study of the PBE Cycle 100kN LH2/LO2 Rocket Engine
Author/Editor: 苅田, 丈士
若松, 義男
橋本, 亮平
冠, 昭夫
KANDA, Takeshi
WAKAMATSU, Yoshio
HASHIMOTO, Ryohei
KANMURI, Akio
Author Heading: 苅田, 丈士
若松, 義男
橋本, 亮平
冠, 昭夫
KANDA, Takeshi
WAKAMATSU, Yoshio
HASHIMOTO, Ryohei
KANMURI, Akio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1988-03
Publication Date (W3CDTF): 1988-03
Alternative Title: PBEサイクル100kN級のLH2/LO2ロケットエンジンの検討
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-965
No. or year of volume/issue: 965
Volume: 965
Pages: 20-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): 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.
資料番号: NALTR0965000
レポート番号: NAL TR-965
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ