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Spacecraft Power Systems

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Presentation on theme: "Spacecraft Power Systems"— Presentation transcript:

1 Spacecraft Power Systems

2 Spacecraft Power Systems
Power Source Table compares common s/c power sources Photovoltaic Cells Cell types Sizing (Peak and Average Power) Radiation Environment Thermal Environment Shadowing Mission life Degradation characteristics

3 Spacecraft Power Systems
Power Source Radioactive Power Sources Radioisotope Thermoelectric Generators (RTGs) Nuclear Reactor Dynamic Power Sources Brayton, Stirling, Rankine cycles Fuel Cells Energy from oxidation reactions High efficiency, short duration missions

4 Spacecraft Power Systems
Energy Storage Physical Constraints Size Mass Operating position Static and dynamic environments Programmatic Constraints Cost Mission Power required, eclipse frequency and length Reliability Maintainability

5 Spacecraft Power Systems
Energy Storage Electrical Constraints Voltage Current Loading Duty cycles (length and frequency) Depth of discharge Activation time

6 Spacecraft Power Systems
Power Distribution Cabling 10-25% of power system mass Volume and location constraints Fault Protection Detection Isolation Correction Switching Subsystems require different amounts of power at different times Power from batteries, arrays, RTG’s etc.

7 Spacecraft Power Systems
Power Regulation and Control Peak Power Tracking (PPT) Non-dissipative DC-DC converter in series with solar arrays Direct Energy Transfer (DET) Dissipative Shunt regulator in parallel with arrays


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