This invention relates to a
detector support structure, specifically a space
payload detector support structure and installation method that combines
vibration isolation and heat dissipation. It primarily addresses the technical problem that existing
detector support structures cannot simultaneously solve the
vibration isolation and heat dissipation issues of space
payload detectors. The structure includes a
heat sink, a flexible heat-conducting cable, a heat-conducting plate, and a bracket. The
heat sink is connected to the
temperature control surface of the external space
payload. One end of the flexible heat-conducting cable is connected to the
heat sink, and the other end is connected to the heat-conducting plate. The heat-conducting plate has a glue injection groove, a temperature probe mounting groove, and a fixing hole on its end face. The detector circuit board and the detector body are respectively disposed on the upper and lower end faces of the heat-conducting plate, and the detector pins are connected to corresponding holes on the detector circuit board. The temperature probe is installed in the temperature probe mounting hole. The bracket is connected to both the detector circuit board and the external optical platform. This detector support structure effectively combines
vibration isolation and heat dissipation.