@inproceedings{oai:jaxa.repo.nii.ac.jp:00038766,
 author = {青木, 良尚 and 石本, 真二 and Aoki, Yoshihisa and Ishimoto, Shinji},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県, An arc-heated wind tunnel test was conducted to confirm the measurement method of stagnation pressure on JAXA lightweight ablator in JAXA 750 kW Arc-heated Wind Tunnel. In this test we confirmed pressure measurement system installed on the small size re-entry capsule will work and this will not cause ablator breaks. And we found two problems for more accurate measurement: 1) the influences of ablator recession around pressure port and 2) ablator-gas on the measurement., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600022000, レポート番号: JSASS-2015-4635},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {JAXA軽量アブレータ表面のよどみ点圧力計測},
 year = {2015}
}