High chamber pressure test for Lox/EA rocket engine and hydrocarbon propellant R&D plan
| Autor: | Hiraiwa, Tetsuo, Azuma, Nobuyuki, Sugimori, Taizo, Tadano, Makoto, Satou, Masahiro, Tomita, Takeo |
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| Jazyk: | japonština |
| Rok vydání: | 2013 |
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| Zdroj: | 第57回宇宙科学技術連合講演会講演集 = Proceedings of 57th Space Sciences and Technology Conference. |
| Popis: | 第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県 As for future, sustainable propellant, hydrocarbon, especially ethanol fuel has been studied in JAXA space transportation mission directorate. Early this year, high chamber pressure test had started with impinging fuel injectors in step with other fundamental investigation and system researches. This paper shows this outline and some firing-test results with high chamber pressure. 資料番号: AC1400020000 レポート番号: JSASS-2013-4273 |
| Databáze: | OpenAIRE |
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