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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.

Storage Temp (deg C) 0 –30 0 –50 0 –10 0 –30 Storage Life 30-90 days wet, 5 yr dry 10 yr 2 yr 5 yr Open circuit voltage(V/cell) 1.6 3.0 3.0 3.6 Discharge voltage(V/cell) 1.5 2.7 2.5 3.2 Manufacturers Eagle Pitcher, Yardley Honeywell, Power Conver Eagle Pitcher Duracell, Altus, ITT

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  Storage, Mit opencourseware, Opencourseware, Spacecraft

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