Status: Completed
Start Date: 2016-08-01
End Date: 2018-08-01
This project will develop a CubeSat integrated structural battery. With structural elements of graphitic and carbon fiber electrodes in an electrolytic polymer, the multifunctional capacitive energy system can serve as both a lightweight load bearing structure and an electrochemical battery system. Multifunctional material can reduce mass and increase electrical power in highly integrated small spacecraft.
In addition to reduced mass and increase electrical power in small spacecraft, structural battery materials are applicable to multiple future missions and commercial applications with other highly integrated systems including drones, electric aircraft, robotic exploration systems, and ruggedized sensors.
Lead Organization: University of Miami