The project is about simulating, modeling and designing solar panels for a 3U CubeSat and with the major objective of achieving maximum efficiency. As these solar panels are the main source of power delivered to all the satellite's subsystems, the design will provide input to the power conditioning
Solar Panel Design for CubeSat
The project is about simulating, modeling and designing solar panels for a 3U CubeSat and with the major objective of achieving maximum efficiency. As these solar panels are the main source of power delivered to all the satellite's subsystems, the design will provide input to the power conditioning and distribution in order to provide a stable output voltage to satellite subsystems. Furthermore, we also investigate the integrated printed magnetometers to be placed inside the solar panel unit for satellite attitude control.
Direct:
Indirect:
The final deliverables of the project will be:
| Item Name | Type | No. of Units | Per Unit Cost (in Rs) | Total (in Rs) |
|---|---|---|---|---|
| Micro-controller | Equipment | 10 | 500 | 5000 |
| Discrete RLC components | Equipment | 50 | 30 | 1500 |
| Current/Voltage /temperature sensors | Equipment | 6 | 500 | 3000 |
| Triple junction solar cells | Equipment | 7 | 8000 | 56000 |
| Adhesives | Equipment | 7 | 500 | 3500 |
| LCD’s | Equipment | 5 | 200 | 1000 |
| Miscellaneous | Miscellaneous | 10 | 1000 | 10000 |
| Total in (Rs) | 80000 |
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