The National Aeronautics and Space Administration (NASA) and the Air Force Research Laboratory (AFRL) are cooperating under a space act agreement to sponsor the research and development of aerospace flywheel technologies to address mutual future mission needs. Flywheel technology offers significantly enhanced capability or is an enabling technology. Generally these missions are for energy storage and/or integrated power and attitude control systems (IPACS) for mid-to-large satellites in low earth orbit. These missions require significant energy storage as well as a CMG or reaction wheel function for attitude control. A summary description of the NASA and AFRL flywheel technology development programs is provided, followed by specific descriptions of the development plans for integrated flywheel system tests for IPACS applications utilizing both fixed and actuated flywheel units. These flywheel system development tests will be conducted at facilities at AFRL and NASA Glenn Research Center and include participation by industry participants Honeywell and Lockheed Martin.
Aerospace Flywheel Technology Development for IPACS Applications
36th Intersociety Energy Conversion Engineering Conference ; 2001 ; Savannah, GA, United States
2001-10-01
Report
No indication
English
Single Axis Flywheel IPACS 1300W, 0.8 N-m
NTIS | 2005
|Single Axis Flywheel IPACS @1300W, 0.8 N-m
NTRS | 2005
|Flywheel Technology Development Program for Aerospace Applications
British Library Conference Proceedings | 1997
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