Electric Power Systems Flashcards
Primary Energy Sources: (4)
- Used for generating power supply during sunlight periods (continuously)
- Photovoltaic
- Heat Conversion using a thermoelectric generator
- For short times: Fuel cell and battery
Secondary Energy Sources: (Def, 3 examples)
- Used mainly for power storage
- Ex:
• Rechargeable batteries
• Regenerative fuel cells
• Solar dynamic generator
Primary Energy Sources Characteristic: Photovoltaic (4):
- Sunlight freely available
- Around Earth: ~1360 W/m^2
- Reduces with ~ r^2 (distance from Sun)
- Mars/Jupiter is informal “boundary” for the usefulness of solar cells
For a given solar cell, the power output depends on: (4)
- Illumination level (distance from the sun)
- Projected area
- Level of degradation (radiation)
- Temperature
Radiation - Lifetime limiting factors (5):
- Main Reason for degradation
- Si-based cells have a lower sensitivity to radiation than others. GaAs is even better!
- n-type is always on top since less sensitive to radiation
- Thin cells are less sensitive to radiation
- Use glass covers for radiation and environmental protection
When sizing a solar array one has to keep in mind of: (3)
- End of Lifetime (EOL) power generation is lower than the Begin of Lifetime (BOL)
- Spacecraft might move in areas with higher or lower illumination
- Power Consumption of a spacecraft might change during the mission
Primary Sources: Solar Dynamic Generators [Def, Pro, Con]
-> Any power sources working with Stirling, Rankine, or Brayon cycles.
• PRO: Higher specific power generation, smaller deployment structures
• CON: Moving parts & Dependence of Sun alignment
Primary Sources: Radioisotope Thermoelectric Generator (RTG) [Def, Pro, Con]
-> Use radioactive decay to generate heat
• PRO: No sun dependency, no moving parts
• CON: Low efficiency (5-7%), huge initial energy dissipation
Primary Sources: Nuclear Reactor [Def]
-> Fission of heavy elements like uranium‐235 creates heat which is
converted to electricity
• Used as a propulsion mean
• Generates contamination and space debris
Secondary source: Batteries [Def]
-> Storage of electrothermal energy to release electrical power
• Preferred for photovoltaic primary sources
• Short supply time
Secondary source: Fuel Cells [Def]
-> Converts H2 and O2 into H20 – releases electrical power
• Water can be consumed by astronauts
• More complex than batteries
Power Management - Voltage and power output can be regulated by (5):
‐ Maximum Power Point Tracking (PPT or MPPT)
‐ Pulse‐width modulation
‐ Sequential Switching Shunt Regulation (S3R)
‐ Direct Energy Transfer (DET)
‐ Individual DC‐DC transformer are also standard
Power Management - EPS Components (6):
- Solar Power Assemblies (SPA)
- Mode Control Unit (MCU)
- Power Control and Distribution Unit (PCDU)
- Battery Management Unit (BMU)
- Battery Charge Regulator (BCR)
- Battery Discharge Regulator (BDR)