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)