Research Mission: The goal of Spacecraft Thermal Management Systems (STMS) is to be developing several Variable Emissivity Device prototypes, or VEDs, one of which is to be applied as payload to a CubeSat and launched into Low-Earth Orbit. This VED will mitigate thermal loads from the sun and internal satellite electronics and offers a low-cost thermal control solution to absorb or reject heat from spacecraft. We work closely with the UCI CubeSat project to coordinate the VED and satellite operations.
