@inproceedings{oai:jaxa.repo.nii.ac.jp:00003691,
 author = {吉尾, 颯 and 奥山, 圭一 and 下田, 孝幸 and Szasz, Bianca and 加藤, 純郎 and Yoshio, Hayato and Okuyama, Keiichi and Shimoda, Kazuyuki and Szasz, Bianca and Kato, Sumio},
 book = {宇宙航空研究開発機構特別資料: 第12回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 12th Spacecraft Environment Symposium},
 month = {Mar},
 note = {第12回 宇宙環境シンポジウム（2015年11月16日-18日. 北九州国際会議場　国際会議室）, 北九州市, 福岡県, The 12th Spacecraft Environment Symposium (November 16-18, 2015. International Conference Room, Kitakyushu International Conference Center), Kitakyushu, Fukuoka, Japan, The LATS (Lightweight Ablator series for Transfer vehicle) is a porous CFRP composite material and it can endure from heat flux bunch of approximately 15 MW/sq m, m2. After a Nano probe finish collecting samples of lunar, they make a reentry into the earth's atmosphere with the speed of 11 km/s without slowdown. This report shows a heat shield system using this LATS. Specifically, this report shows about the heat shield constitution and a necessary thickness, an in-depth temperature history during a re-entry flight., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630004036, レポート番号: JAXA-SP-15-012},
 pages = {347--349},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {月軌道から帰還する超小型プローブの熱防御システム},
 volume = {JAXA-SP-15-012},
 year = {2016}
}