To provide a space environment testing device capable of rotating a temperature controlling plate, reducing occurrence of deficiency of a driving part due to temperature environment and facilitating maintenance.
This space environment testing device 1 is constituted by providing the temperature controlling plate 5 to fix a test piece 4 in a vacuum container 2, providing a rotation axis 6 to rotate the temperature controlling plate 5 penetrating the vacuum container 2 and providing a flexible piping 8 to supply and discharge a refrigerant 7 to and from the temperature controlling plate 5 wound around the rotation axis 6. Additionally, the driving part 30 to rotate and drive the temperature controlling plate 5 from the outside of the vacuum container 2 is provided with the rotation axis 6, and the flexible piping 8 is constituted so as to wind around the rotation axis 6 with rotation of the temperature controlling plate 5.
COPYRIGHT: (C)2007,JPO&INPIT
Nao Kitayama
Wataru Takahashi
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Takashi Watanabe
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