The invention discloses a thermal vacuum and
thermal cycle test
system for a space
micropump, and aims to solve the problems that a medium leaks in a high and low temperature test process of an existing test
system, the space
micropump cannot operate normally after air enters a test loop, and even the test cannot be carried out. The device comprises a thermal circulation
assembly, a transfer injection tank, a connecting piece, a first hand valve, a first pressure gauge, a
vacuum pump, a second hand valve, a second pressure gauge, a pressure
reducer and an air source, the thermal circulation
assembly is connected with the first hand valve and the second hand valve through the connecting piece, the first hand valve is connected with the first pressure gauge through a connecting pipeline, and the first pressure gauge is connected with the
vacuum pump through a pipeline; the second hand valve is connected with a long guide
pipe connector of the transfer injection tank through a pipeline, a short guide
pipe connector of the transfer injection tank is connected with a second pressure gauge through a pipeline, and the second pressure gauge is connected to a pressure
reducer which is connected with an air source. The sealing device is simple in structure, easy to
machine and high in sealing reliability. The device is used for high and low temperature
test performance testing of the space
micropump and the pump valve
assembly.