Deployable telescopic radiative system for space system e.g. satellite, has heat sink assemblies including radiators mounted to be movable such that heat sink assemblies are connected in series when system is in deployed position

摘要

The system has a main heat sink assembly (10) including a radiator (11) and another radiator, an intermediate heat sink assembly (20) including two radiators, and a secondary heat sink assembly (30) including two radiators. The radiators of the heat sink assemblies are mounted to be movable such that the heat sink assemblies are concentric when the system is in stored position, and the heat sink assemblies are connected in series when the system is in deployed position. An independent claim is also included for a space system.