Design and verification of elongated load installation for a spacecraft

LinXin Wang; YaJun Hong; Qilong Zhao; Hanwu Liu; Ce Jiang

doi:10.1117/12.3030284

5 June 2024 Design and verification of elongated load installation for a spacecraft

LinXin Wang, YaJun Hong, Qilong Zhao, Hanwu Liu, Ce Jiang

Proceedings Volume 13163, Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024); 1316303 (2024) https://doi.org/10.1117/12.3030284
Event: International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024), 2024, Xi'an, China

Abstract

When the payload on a spacecraft is installed with the platform, a suitable installation mode should be designed according to the shape of the payload to ensure the reliable connection between the payload and the platform. The payload installed on a spacecraft is elongated. Based on the analysis of the characteristics of this type of payload, this paper designs a installation method between it and the platform, and designs an installation gap adjustment mode. After the installation is completed, the installation can be judged whether the installation is in place by detecting the installation gap between the payload and the platform. The reasonableness and reliability of the designed installation mode are verified by mechanical tests. The test results show that the designed loading installation mode meets the mechanical requirements.

(2024) Published by SPIE. Downloading of the abstract is permitted for personal use only.

Citation Download Citation

LinXin Wang, YaJun Hong, Qilong Zhao, Hanwu Liu, and Ce Jiang "Design and verification of elongated load installation for a spacecraft", Proc. SPIE 13163, Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024), 1316303 (5 June 2024); https://doi.org/10.1117/12.3030284

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