The MVP System from CU Aerospace LLC is an Electrothermal Thruster that has a thrust of 0.0045 N. It is well-suited for 3U or larger CubeSats. This spacecraft thruster has a mass of 1.06 Kg and a specific impulse of 66 sec. It has a power consumption of 13.5-45 W and requires a supply voltage of 12 V. This thruster supports RS-422 and RS-232 interfaces. It consumes an inert polymer propellant fiber which is a patented technology that retains performance characteristics competitive with other warm gas systems.
