NOVELTY - An embedding insert (3) arranged at desired position is temporarily fixed with adhesive agent (13), on layered structure of lower panel epidermis (4a) and film adhesive (5a). A honeycomb core (2) and formwork jig (14) arranged on layered structure are sequentially laminated with film adhesive (5b) and upper panel epidermis (4b) and forms a pattern (1a) of honeycomb sandwich panel which is shaped.    USE - For shaping of insert embedding type honeycomb sandwich panel for solar cell panel of satellites.    ADVANTAGE - The shaping method of insert embedding type honey-comb sandwich panel restrains the deviation of dislocation of embedding insert.    DETAILED DESCRIPTION - A bottom board, lower panel epidermis and film adhesive (5a) are sequentially laminated on a fixed board and forms the layered structure. The embedding insert is arranged at desired position on the layered structure and temporarily fixed with normal temperature adhesive agent. The honey-comb core is arranged on the layered structure and the frame-like formwork jig is arranged at the periphery of honeycomb core. The film adhesive (5b) and upper panel epidermis are sequentially arranged on the formwork jig and forms a pattern of honeycomb sandwich panel. A pushing board, a release film and a ventilation cloth are further stacked on the pattern, and the whole is covered with a vacuum bag film. The whole vacuum bag in the sealed state is heated and pressurized. The panel is then picked out from the formwork jig and the insert embedding type honeycomb sandwich panel is shaped.    DESCRIPTION OF DRAWING(S) - The figure shows the formation process of insert embedding type honeycomb sandwich panel. (Drawing includes non-English language text).    pattern of insert embedding type honeycomb sandwich panel (1a)    honeycomb core (2)    embedding insert (3)    lower panel epidermis (4a)    upper panel epidermis (4b)    film adhesives (5a,5b)    normal temperature adhesive agent (13)    formwork jig (14)