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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.

diameter by 15.9-in. in length – Delivers 2 kW-hr of useful energy for a typical 37-minute LEO eclipse cycle – high speeds of up to 60,000 rpm • the current average for commercial GSO storage is 2,400 lbs of batteries, which is decreased to 720 lbs with an equivalent FESM. • Honeywell has developed an integrated flywheel

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