LH2/LO2 Rocket Engine with Solar Energy

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: 1988-08

Material Format: Digital

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Note (General)：: Solar energy is already used in the form of electric power generated by solar cells in satellites. And a solar thermal propusion system, a kind of gas...

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Material Type: 文書・図像類
Title: LH2/LO2 Rocket Engine with Solar Energy
Author/Editor: 苅田, 丈士
若松, 義男
冠, 昭夫
KANDA, Takeshi
WAKAMATSU, Yoshio
KANMURI, Akio
Author Heading: 苅田, 丈士
若松, 義男
冠, 昭夫
KANDA, Takeshi
WAKAMATSU, Yoshio
KANMURI, Akio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1988-08
Publication Date (W3CDTF): 1988-08
Alternative Title: 太陽熱を利用した小型液酸/液水ロケットエンジン
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-992
No. or year of volume/issue: 992
Volume: 992
Pages: 12-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): Solar energy is already used in the form of electric power generated by solar cells in satellites. And a solar thermal propusion system, a kind of gas jet engine, has been studied. Large expansion area engines have been studied to achieve high specific impulse, Isp. If external energy is added to an engine, Isp can be better than the theoretical Isp based on tank level enthalpy. In this report, solar energy was used as the additional energy supplied to a rocket engine. The LH2/LO2 expander cycle engine with a solar heat exchanger was studied. This engine has two merits. One is the increase of Isp, which allows a greater payload to be carried by a rocket with the solar heat exchanger than by a normal rocket. The other merit is a cycle pressure level decrease. The Isp increase is realized for every engine and for every propellant, if additional energy is available.
資料番号: NALTR0992000
レポート番号: NAL TR-992
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45251&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45251&item_no=1&attribute_id=31&file_no=1
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