PROBLEM TO BE SOLVED: To provide a space device adapter, a space transport aircraft, and an artificial satellite capable of achieving both desired rigidity and weight saving.SOLUTION: A space device adapter 100 that supports a space device inside a transport aircraft with respect to an aero-space is configured by annularly joining a plurality of split bodies 13, and characterized in that each split body has a through-hole 130 that penetrates a plate-like member constituting the split body in a thickness direction, and a rib structure 135 that is formed by a part of the plate-like member so as to surround the opening of the through-hole at the opening peripheral edge of the through-hole.SELECTED DRAWING: Figure 1
【課題】所望の剛性を確保しつつ軽量化を併せて実現できる宇宙機器アダプタ及び宇宙輸送機並びに人工衛星を提供する。【解決手段】宇宙空間に対する輸送機の内部で宇宙機器を支持する宇宙機器アダプタ100であって、複数の分割体13を環状に接合することで構成され、前記分割体の各々は、前記分割体を構成する板状部材を厚さ方向に貫通する貫通孔130と、前記貫通孔の開口周縁部において前記貫通孔の開口を取り囲むように前記板状部材の一部で形成されたリブ構造部135とを有することを特徴とする宇宙機器アダプタ。【選択図】図1
SPACE DEVICE ADAPTER, SPACE TRANSPORT AIRCRAFT, AND ARTIFICIAL SATELLITE
宇宙機器アダプタ及び宇宙輸送機並びに人工衛星
2018-03-08
Patent
Electronic Resource
Japanese
IPC: | B64G Raumfahrt , COSMONAUTICS |
SPACE MEDICAL DEVICE, SPACE MEDICAL METHOD, AND ARTIFICIAL SATELLITE
European Patent Office | 2021
|European Patent Office | 2021
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