The UCI Spacecraft Thermal Management Team is designing a Variable Emissivity Radiator utilizing an electrochromically controlled film to regulate the temperature of a 2-unit CubeSat in polar low earth orbit.
Project Definition
Project Specification
Advisors
Project Team
Amy Dunford
Graduate Student Project Lead
Nicholas Cordero
CubeSat-III Thermal Lead (Aerospace Engineering)
Noah McFerran (Chemical Engineering)
Raymond Jess Duenas (Mechanical Engineering)
Abdullaah Tarif
Software Team Lead (Aerospace Engineering)
Michael Beck (Aerospace Engineering)
Brian Nguyen (Aerospace Engineering)