 Flywheel Integrated Power and Attitude Control System Demonstrated by NASA Glenn Research Center

In Research & Technology 2005, NASA/TM-2006-214016, published1May2006; institutional record 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.