| contributor author | Zhang, Wei | |
| contributor author | Zhang, Shijie | |
| contributor author | Dong, Zezheng | |
| contributor author | Wang, Haibo | |
| contributor author | Yang, Dalin | |
| contributor author | Chen, Ming | |
| contributor author | Liu, Xiangzhen | |
| date accessioned | 2026-08-20T21:13:50Z | |
| date available | 2026-08-20T21:13:50Z | |
| date copyright | 2025/11/18 | |
| date issued | 2026 | |
| identifier other | JAEEEZ.ASENG-6304.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314152 | |
| description abstract | AbstractThis paper proposes a rigid–flexible–thermal coupling dynamics model for a spacecraft
with a composite-laminated solar array in a space thermal environment, and the thermally
induced vibration on the spacecraft is studied. The spacecraft system ... | |
| publisher | American Society of Civil Engineers | |
| title | Rigid–Flexible–Thermal Coupling Dynamics for Spacecraft with a Composite-Laminated Solar Array in a Space Thermal Environment | |
| type | Journal Article | |
| journal volume | 39 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/JAEEEZ.ASENG-6304 | |
| journal fristpage | 04025123-1 | |
| journal lastpage | 04025123-22 | |
| page | 22 | |
| tree | Journal of Aerospace Engineering:;2026:;Volume ( 039 ):;issue: 002 | |
| contenttype | Fulltext | |
