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The open core composite flywheel
IECEC-97 Proceedings of the Thirty-Second Intersociety Energy Conversion Engineering Conference (Cat. No.97CH6203)
In low earth orbit satellite applications, spacecraft power is provided by photovoltaic cells and batteries. Unfortunately, use of batteries present difficulties due to their poor energy density, limited cycle lifetimes, reliability problems, and the difficulty in measuring the state of charge. Flywheel energy storage offers a viable alternative to overcome some of the limitations presented by batteries. This paper discusses the University of Maryland's operational 300 Wh open core composite
doi:10.1109/iecec.1997.656686
fatcat:b6yccn7tmbhwdmvjdye6lvey3i