Conference Paper 月軌道から帰還する超小型プローブの熱防御システム
A Heat Shield System of a Nano-Sized Space Probe Returning from a Lunar Orbit

吉尾, 颯  ,  奥山, 圭一  ,  下田, 孝幸  ,  Szasz, Bianca  ,  加藤, 純郎  ,  Yoshio, Hayato  ,  Okuyama, Keiichi  ,  Shimoda, Kazuyuki  ,  Szasz, Bianca  ,  Kato, Sumio

Description
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.
会議情報: 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
形態: カラー図版あり
Meeting Information: 12th Spacecraft Environment Symposium (November 16-18, 2015. International Conference Room, Kitakyushu International Conference Center), Kitakyushu, Fukuoka, Japan
Physical characteristics: Original contains color illustrations
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https://repository.exst.jaxa.jp/dspace/bitstream/a-is/562155/1/AA1630004036.pdf

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