The invention discloses a surge current suppression circuit of a
spacecraft switch control path. A parallel
branch is formed by connecting a
resistor and a
relay contact in series, and two ends of the parallel
branch are connected with two ends of a power switch K1 contact in parallel. The
relay drive circuit is located at the front end of the power switch drive circuit, the positive end of the secondary
bus is connected with the positive end of a coil of a
relay switch K2 through a current-limiting
resistor, and the negative end of the coil of the relay switch K2 is directly connected with a drive
signal end. The power switch
driving circuit adopts an MOS tube
driving circuit to perform on-off control and adopts a
triode delay circuit to perform
delay control, the positive end of the secondary
bus is connected with the s pole of an MOS tube, the d pole of the MOS tube is connected with the positive end of a coil of the power switch K1 through a current-limiting
resistor of the power switch K1, and the negative end of the coil of the power switch K1 is directly connected with the negative end of the secondary
bus. When the driving
signal is a closing instruction, the relay contact is closed before the power switch contact; and when the driving
signal is a turn-off instruction, the relay contact is disconnected before the power switch contact.