| dc.contributor.author | Xu, Yu | |
| dc.contributor.author | Zhang, Rui | |
| dc.contributor.author | Hu, Siqi | |
| dc.contributor.author | Ma, Errui | |
| dc.contributor.author | Shi, Chenguang | |
| dc.contributor.author | Huang, Hai | |
| dc.date.accessioned | 2026-08-20T21:13:38Z | |
| dc.date.available | 2026-08-20T21:13:38Z | |
| dc.date.copyright | 2025/08/22 | |
| dc.date.issued | 2025 | |
| dc.identifier.other | JAEEEZ.ASENG-6259.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4314146 | |
| dc.description.abstract | AbstractTo address the critical challenges of carrying efficiency and separation safety in
multisatellite launches, an L-shaped satellite configuration with a specialized release
mechanism is proposed. This design maximizes the use of space within the ... | |
| dc.publisher | American Society of Civil Engineers | |
| dc.title | Design and Analysis of an L-Shaped Micro–Nano Satellite and Its Semi-Embedded Lateral Separation Mechanism | |
| dc.type | Journal Article | |
| dc.journal.volume | 38 | |
| dc.journal.issue | 6 | |
| dc.journal.title | Journal of Aerospace Engineering | |
| dc.identifier.doi | 10.1061/JAEEEZ.ASENG-6259 | |
| dc.journal.fristpage | 04025092-1 | |
| dc.journal.lastpage | 04025092-16 | |
| dc.page | 16 | |
| dc.tree | Journal of Aerospace Engineering:;2025:;Volume ( 038 ):;issue: 006 | |
| dc.contenttype | Fulltext | |
