Aerodynamic force and moment computations for very low Earth orbit satellites using a TPMC model
The recent upswing in satellite operations of very low Earth orbit has triggered the necessity to evaluate aerodynamic forces and moments, which can significantly affect satellite orbit. The present paper evaluates the aerodynamic forces and pitching moment on a satellite design using the test parti...
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| Main Authors: | , , , |
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| 其他作者: | |
| 格式: | Article |
| 語言: | English |
| 出版: |
2025
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| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/182134 |
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| 機構: | Nanyang Technological University |
| 語言: | English |