Motor/generator and electronic control considerations for energy storage flywheels

Details Motor/generator and electronic control considerations for energy storage flywheels Motor/generator and electronic control considerations for energy storage flywheels

Nov 1984

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984aifs.nasa..389n&link_type=abstract

In NASA. Langley Research Center An Assessment of Integrated Flywheel System Technol. p 389-406 (SEE N85-13850 05-20)

Physics

Electric Generators, Electric Motors, Electronic Control, Energy Storage, Flywheels, Spacecraft Power Supplies, Lunar Surface Vehicles, Pulse Duration Modulation, Solar Generators

Scientific paper

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.

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