公开(公告)号：US20050151021A1

公开(公告)日：2005-07-14

申请号：US10740294

申请日：2003-12-17

申请人： Douglas Hamilton ,  Patrick Alsup ,  Theresa Alsup

发明人： Douglas Hamilton ,  Patrick Alsup ,  Theresa Alsup

IPC分类号： B64G1/50 ,  B64G1/46

CPC分类号： B64G1/503

摘要： A heat-dissipating, light-reflecting plate for a radiator of a spacecraft is provided. The heat-dissipating, light-reflecting plate has an at least partially transparent, thermally conductive layer and a plurality of first light-reflecting surfaces disposed proximate to the at least partially transparent, thermally conductive layer. A plurality of second light-reflecting surfaces also is disposed proximate to the at least partially transparent, thermally conductive layer. At least a first sub-set of the plurality of second light-reflecting surfaces is oriented at a first angle to at least a first sub-set of the plurality of first light-reflecting surfaces.

摘要翻译： 提供了一种用于航天器散热器的散热光反射板。 散热光反射板具有至少部分透明的导热层和靠近该至少部分透明的导热层设置的多个第一光反射表面。 多个第二光反射表面也设置在至少部分透明的导热层附近。 所述多个第二光反射面的至少第一子集与所述多个第一光反射面的至少第一子集成第一角度。