The invention provides a
satellite thermal vacuum test ground power supply
system. A solar
simulation array converts a three-phase
alternating current into a
constant current source for providing a charging power supply to a
satellite; a launching control platform carries out on-off control and state monitoring on a charging link and simultaneously collects voltages of storage batteries and platform buses on the
satellite; an external transit
cable network divides the charging power supply into two paths, wherein one path is connected to sliding rings of the satellite through a
flange disk and an internal transit
cable network, and then output power is connected to a diverter and a
charge and discharge regulator of the satellite through sliding ring channels; and the other path is connected to a pull-off plug through the
flange disk and the internal transit
cable network, and then output power is connected to the diverter and the
charge and discharge regulator through pull-off plug channels, so that standby channels are available for supplying power to the satellite when the sliding rings break down, the battery
discharge depth of the satellite does not exceed a designed value, and a thermal vacuum
simulation test can be continued. The satellite thermal vacuum test ground power supply
system is simple in structure, an existing
system is changed a little, and proved by experiments, the method is reasonable and feasible.