| 摘要 |
PROBLEM TO BE SOLVED: To solve the problem that troublesome labor is required for fabrication, there is a limit in the point of reduction weight, and the maximum thermal deformation of 5μm causes the deformation of a reflecting mirror to possibly put a telescope into an unfocused condition and preclude the mounting of optical equipment having high resolution. SOLUTION: This honeycomb sandwiched panel for satellite mounted optical equipment comprises a honeycomb core and a skin for covering both-side surfaces of the honeycomb core, the honeycomb core and the skin being formed of CFRP. It also has an outside honeycomb core arranged on a portion to which a heavier load is applied than to other portions and an inside honeycomb core lighter than the outside honeycomb core, which is arranged on a portion excluding the outside honeycomb core.
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