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.
Design and verification of elongated load installation for a spacecraft
Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024) ; 2024 ; Xi'an, China
Proc. SPIE ; 13163
2024-06-05
Conference paper
Electronic Resource
English
Spacecraft thermocouple installation design.
NTRS | 1964
|METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE
European Patent Office | 2016
|METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE
European Patent Office | 2016
|METHOD FOR UNIAXIAL ORIENTATION OF SPACECRAFT WITH ELONGATED SHAPE
European Patent Office | 2016
|Spacecraft thermal design verification through modeling
NTRS | 1971
|