| 摘要 |
PROBLEM TO BE SOLVED: To provide a radiator panel for a spacecraft that has small mass and/or has a small thickness.SOLUTION: A radiator panel includes at least one insert 106 arranged adjacent to a heat pipe 108 between two spaced-apart face sheets 42 and 44. The insert is configured so that a package 52 is secured to an inside face sheet opposite to the heat pipe. Some radiator panels 100 include at least one external structural reinforcement member extending across an external side of an outside face sheet 44 of the radiator panel. |
