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    Motor/generator and electronic control considerations for energy storage flywheels (1984)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: A spacecraft electric power supply system is described. Requirements of the system are to accelerate a momentum wheel to a fixed maximum speed when solar energy is available and to maintain a constant voltage on the spacecraft bus under varying loads when solar energy is not available. Candidate motor types, pulse width modulated current control systems, and efficiency considerations are discussed. In addition, the Lunar Roving Vehicle motors are described along with their respective efficiencies.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
    Type: NASA. Langley Research Center An Assessment of Integrated Flywheel System Technol.; p 389-406
    Format: application/pdf
    Location Call Number Expected Availability
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