Electronic Resource
将来輸送系リファレンスシステムの推進系に関する基礎検討
| العنوان: | 将来輸送系リファレンスシステムの推進系に関する基礎検討 |
|---|---|
| Additional Titles: | Basic Study on the Propulsion System of Future Transportation Reference System |
| المؤلفون: | 笹木 康平, 飯島 明日香, 中田 大将, 湊 亮二郎, 棚次 亘弘, 杉岡 正敏, 東野 和幸, 石本 真二, 東 伸幸 |
| بيانات النشر: | 室蘭工業大学 2015-03-13 |
| نوع الوثيقة: | Electronic Resource |
| مستخلص: | The feasibility of GG cycle reusable rocket engine is examined in this study based on the requirements of JAXA reference mission. Bioethanol is used as fuel and LOX is used as oxidizer. The combustion chamber pressure, the expansion ratio and the fuel injection temperature are set to 7 MPaA, 25 and 390 K. As a result, 0.6 in its turbine/pomp efficiency and 0.954 in its Isp efficiency are needed to satisfy the mission requirements. Besides, the experimental study was conducted to confirm the validity of anticorrosion coating on A6061 alloy in high-pressure and high-temperature ethanol. 特集 : 航空宇宙機システム研究センターにおける開発研究2 : 1. オオワシII飛行にむけて並びに関連技術の研究開発（推進系） |
| مصطلحات الفهرس: | Bioethanol, Reusable Rocket Engine, GG Cycle, Anti-Corrosion Coating, 538, Departmental Bulletin Paper |
| URL: | |
| الاتاحة: | Open access content. Open access content © 2015 室蘭工業大学 |
| ملاحظة: | application/pdf 室蘭工業大学紀要 = Memoirs of the Muroran Institute of Technology, 64, 3-8(2015-03-13) Japanese |
| Other Numbers: | YL# oai:muroran-it.repo.nii.ac.jp:00008565 https://muroran-it.repo.nii.ac.jp/?action=repository_uri&item_id=8565 室蘭工業大学紀要 = Memoirs of the Muroran Institute of Technology, 64, 3-8(2015-03-13) 13442708 AA11912609 https://muroran-it.repo.nii.ac.jp/?action=repository_action_common_download&item_id=8565&item_no=1&attribute_id=24&file_no=1 1137562055 |
| المصدر المساهم: | MURORAN INST OF TECH From OAIster®, provided by the OCLC Cooperative. |
| رقم الانضمام: | edsoai.on1137562055 |
| قاعدة البيانات: | OAIster |
| الوصف غير متاح. |