Spacecraft, particularly satellite, for mission, is moved on path with alignment to sun radiation and is moved on another path with another alignment to sun radiation, where radiator dissipated heat from interior of spacecraft in universe

摘要

The spacecraft (1) is moved on a path with an alignment to sun radiation and is moved on another path with another alignment to the sun radiation. A radiator (15) is provided for dissipating the heat from the interior of the spacecraft in the universe (13). The radiator is held from a base body (14) of the spacecraft. A compensation element is mounted to the radiator and is inclined opposite to the radiator such that a compensation body (17) is acted on the former path with the alignment with the sun radiation then on the latter path with the latter alignment.