Structural Design Modification of a CubeSat Regarding Modal Compatibility for Launching by Vega C Launcher
In this research, the dynamic response of a U-12 CubeSat (20x20x30 cm) is investigated for three configurations during the launch conditions. Despite the existence of a successful design for this satellite, adding a mount to install on a standard adapter, the structural design of the satellite has b...
| Main Authors: | , , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2023-12-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_176736_eaaf927d575c8430b67e4c3b6b0ac1cb.pdf |