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Spacecraft Power Systems - MIT OpenCourseWare

Spacecraft Power Systems David W. Miller John Keesee Electrical Power System EPS. Power energy Power Power Regulation Source storage Distribution and Control Power Sources Primary Batteries Radioisotope Secondary Battery Thermionic converter Fuel cell Thermoelectric converter Regenerative fuel cell Photovoltaic Chemical dynamic Solar dynamic Nuclear flywheel storage Electrodynamics Tethers Propulsion-charged tether Power Source Applicability 100. NUCLEAR THERMIONICS. SOLAR DYNAMIC AND. FUEL CELL PHOTOVOLTAIC. NUCLEAR. LOAD Power (kW). 10. CHEMICAL. DYNAMIC. (APUs) NUCLEAR THERMIONIC. OR SOLAR DYNAMIC. PHOTOVOLTAIC OR. 1 ISTOTOPE - THERMOELECTRIC. PRIMARY MONTHS YEARS. BATTERIES. 1 DAY 10 DAYS 1 2 3 6 12 2 4 6 810. 1 10 100 103 104 105. HOURS. Approximate ranges of application of different Power sources.

Flywheel Energy Storage Modules (FESM) could replace batteries on Earth-orbit satellites. • While in sunlit orbit, the motor will spin the flywheel to a fully charged speed – generator mode will take over to discharge the flywheel and power the satellite during the eclipse phase – present flywheel technology is about four times better

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