JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
63742010.pdf713.3 kB
Other TitleThermal response analysis of low-density ablators
Author(jpn)小林 祐介; 酒井 武治; 奥山 圭一; 鈴木 俊之; 藤田 和央; 加藤 純郎
Author(eng)Kobayashi, Yusuke; Sakai, Takeharu; Okuyama, Keiichi; Suzuki, Toshiyuki; Fujita, Kazuhisa; Kato, Sumio
Author Affiliation(jpn)名古屋大学; 名古屋大学; 津山工業高等専門学校; 宇宙航空研究開発機構 総合技術研究本部; 宇宙航空研究開発機構 総合技術研究本部; 川崎重工業
Author Affiliation(eng)Nagoya University; Nagoya University; Tsuyama National College of Technology; Japan Aerospace Exploration Agency Institute of Aerospace Technology; Japan Aerospace Exploration Agency Institute of Aerospace Technology; Kawasaki Heavy Industries Ltd.
Issue Date2008-02-29
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication title第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集
Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007
Start page56
End page61
Publication date2008-02-29
AbstractThe coking phenomenon within low- density ablative material exposed to aerodynamic heating is studied. The char density of the tested material is measured by slicing the material thinly, and by weighing each of the sliced test pieces. Measured density profiles of the tested materials are compared with the calculated results obtained by a thermal response code. The surface and internal state of both pre- and post- materials are observed by using Scanning Electron Microscope (SEM) and X-ray Computed Tomography (CT). The results show that the measured density profiles is inversely increased to the heated surface. The density increase is likely due to the deposition of a solid carbon in the char region during aerodynamic heating.
DescriptionJAXA Special Publication
Keywordsablation; ablative material; atmospheric entry; aerodynamic heating; coking; weight reduction; thermal response; pyrolysis; carbon-phenolic composite; arc heating; アブレーション; アブレーション材料; 大気圏突入; 空力加熱; コーキング; 軽量化; 熱応答; 熱分解; 炭素-フェノール樹枝複合材料; アーク加熱
Document TypeConference Paper
JAXA Category特別資料
Report NoJAXA-SP-07-016

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.