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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.

The 87-year half-life of Pu-238 results in 96% of the original heat output even after five years Electric - Power Level (kW) Duration of Use 10 MIN 1 HOUR 1 DAY 1 MONTH 1 YEAR 10 YEARS Chemical 10-1 10 0 10 1 10 2 10 3 10 4 10 5 10 6 10 7 Radioisotopes Nuclear reactors Solar

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