DOI: https://doi.org/10.15368/theses.2018.148
Available at: https://digitalcommons.calpoly.edu/theses/1966
Date of Award
12-2018
Degree Name
MS in Electrical Engineering
Department/Program
Electrical Engineering
Advisor
Andrew Danowitz
Abstract
CubeSat designers are increasingly looking to incorporate delicate structures and optics into their payloads. These delicate payloads, however, may not survive the required absolute-worst-case launch vibration testing needed for flight certification. To help address this problem, and to better match testing conditions to real-world launch environments, this thesis introduces Sync, a compact 1/4U CubeSat payload designed to collect data on the vibrations and thermal environments CubeSats experience inside a deployer on the way to orbit. This data can be used to better understand the launch environment for different vehicles, and help develop new, more realistic testing guidelines that could enable more delicate payloads to be launched.
Included in
Acoustics, Dynamics, and Controls Commons, Electrical and Electronics Commons, Other Aerospace Engineering Commons, Space Vehicles Commons