The invention provides a topological structure of a power
supply and distribution system of an all-electric propulsion
satellite. The topological structure comprises a power supply control and distribution unit, an integrated battery, a
solar cell array, a deconcentrator, a load
distributor, an
electrical connection device, at least one group of independent propulsion module batteries, independent propulsion module equipment and ground charging and power supply equipment, the
power control and
power distribution unit adjusts
electric energy and manages power distribution; an integrated battery stores energy and supplies power; the
solar cell array supplies power during illumination; the power
supply and distribution switching process comprises the following steps of: supplying power by a
solar cell array before separation, supplementing an integrated battery in an earth shadow period, and shelving an independent propulsion cabin battery; in the separation conversion stage, the primary
satellite stops supplying power, and the independent propulsion module is powered by a battery and detonated for separation; and after separation, the main
satellite is electrically propelled to transfer orbits to predetermined orbits, and the independent propulsion cabins are powered by batteries to deorbit. Therefore, the
system is suitable for the design of a power
supply and distribution subsystem of a satellite containing a primary satellite and an independent propulsion module, the integration level is high, the single-
machine integration level is large, and
system optimization is simple and reliable.