= Flywheel Integrated Power and Attitude Control System Demonstrated by NASA Glenn Research Center
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https://ntrs.nasa.gov/api/citations/20060054003/downloads/20060054003.pdf
In \i[Research & Technology 2005], NASA/TM-2006-214016, published1May2006; institutional record https://ntrs.nasa.gov/citations/20060054003 . Article locator: Flywheel Integrated Power and Attitude Control System Demonstrated. Opening two paragraphs describe the G2/D1 two-flywheel demonstration, air-bearing table, 20000–60000rpm operating range, simultaneous power-bus regulation and commanded torque. Load-cell measurements determine table torque.
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