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酒井研究室
Showing the original Japanese · View translation
惑星の大気に飛び込む宇宙機の高温の流れを解き明かす研究室。
AboutAbout the lab
大気に突入する宇宙機の熱と流れを解き明かす。
酒井研究室は、
数値解析と
得られた
Key terms
- 極超
音速 - 音の
速さの 5倍ほどを 超える、 とても 速い 流れや 飛行。 機体の まわりの 空気が 高温に なる - アブレーション
- 高温に
さらされた 表面の 材料が、 溶けたり 蒸発したりして 少し ずつ 削られていく 現象 - 熱防御
- 大気に
突入する ときに 生じる 激しい 熱から、 宇宙機の 機体を 守る こと
ResearchResearch themes
惑星大気突入体の
MembersFaculty
- Professor酒井 武治Publications ↗
VoicesStudent voices
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Report an errorAbout the images
The top and research theme images are illustrative and were not taken at the lab. They are cropped from Wikimedia Commons images. Cropped CC BY-SA images are provided under the same CC BY-SA license as the original (version shown on each line).
- Top image: “Progress MS-02 reentry plasma trail” NASA / Public domain (cropped)
- 大気突入体の
熱と 流れ: “Arc Jet Testing of Orion Heat Shield Avcoat (jsc2024e078233)” NASA Ames Research Center / NASA / Public domain (cropped) - Related lab (姫野研究室): “Compressor case from turbojet” Olivier Cleynen / CC BY-SA 3.0 (cropped)
- Related lab (小川・
小田切研究室): “BepiColombo spacecraft model” National Aeronautics and Space Administration (NASA) / Public domain (cropped) - Related lab (津江・中谷研究室): “Combustion research ( )” Oak Ridge National Laboratory / CC BY 2.0 (cropped)
- Related lab (小紫・
小泉研究室): “Hall Effect Thruster in a vacuum chamber” EXOTRAIL SA / CC BY-SA 4.0 (cropped)
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