The invention discloses an
iodine satellite thruster working medium supply
system. The
iodine satellite thruster working medium supply
system comprises a
propellant storage tank, wherein the
propellant storage tank is arranged at the rear end of a thruster and communicates with a main
pipe. The main
pipe is divided into two
branch pipes through a three-way valve. The two
branch pipes are connectedwith a negative pole and a positive pole of the thruster correspondingly. The
propellant storage tank, the main
pipe and the two
branch pipes are each provided with a heating device. The two branch pipes are each provided with a proportional flow
rate control valve. The invention further discloses an application method of the
iodine satellite thruster working medium supply
system. The applicationmethod comprises the specific steps that the propellant storage tank is heated to 90 DEG C, and the main pipe and the branch pipes are each heated to 125 DEG C; and the branch pipe flow rates are controlled through the proportional flow
rate control valves correspondingly, and furthermore, the flow rates of a working medium entering the negative pole and the positive pole of the thruster are controlled. The iodine satellite thruster working medium supply system and the application method thereof have the beneficial effects that the iodine working medium supply system is provided, flow of theiodine working medium can be adjusted through heating, and the system works at the relatively-low temperature; and the system is easy and reliable to apply, and the high
specific impulse and
propulsive efficiency required by propelling of a
cubesat can be continuously generated.