Numerical investigation of solar panel orientation for optimal power generation and drag performance on a VLEO satellite
This research paper delves into the field of small satellites (SmallSats) operations in the very low Earth orbit (VLEO) environment. With orbital altitudes ranging below 450km, the VLEO environment offers numerous advantages for satellite missions in the form of optimising mission performances, redu...
Saved in:
| 主要作者: | |
|---|---|
| 其他作者: | |
| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
Nanyang Technological University
2024
|
| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/176758 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|