Design and dynamic analysis of alpha solar rotary mechanism for China Space Station
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Published:2023-08-14
Issue:10
Volume:95
Page:1531-1541
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ISSN:1748-8842
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Container-title:Aircraft Engineering and Aerospace Technology
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language:en
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Short-container-title:AEAT
Author:
Zhu Jinyao,Niu Cong,Chen Jinbao,Wang Chen,Liu Dianfu,Yang Decai
Abstract
Purpose
The purpose of this study is to describe the proposed alpha solar rotary mechanism (ASRM) and how it is used to accurately modify the solar array of the China Space Station (CSS) in orbit to maintain continuous tracking of the sun to provide power. It also highlights the need to evaluate the performance of the ASRM and predict potential failure modes in various extreme scenarios.
Design/methodology/approach
To evaluate the performance of the ASRM, a dynamic model was created and tested under normal and faulty conditions. In addition, a multidirectional stiffness test was conducted on the prototype to verify the accuracy of the ASRM's dynamic model. The high-precision ASRM model was then used to predict potential failure modes and damaged parts in various extreme scenarios.
Findings
The simulation results were in good agreement with the test results, with a maximum error of less than 8.85%. The high-precision ASRM's model was able to accurately predict potential failure modes and damaged parts in extreme scenarios, demonstrating the effectiveness of the proposed model and simulation evaluation test.
Originality/value
The proposed high-precision ASRM model and simulation evaluation test provide an effective way to evaluate the structural safety and optimize the design of the spacecraft. This information can be used to improve the performance and reliability of the CSS's solar array and ensure continuous power supply to the station.
Subject
Aerospace Engineering
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2. ISS solar array alpha rotary joint (SARJ) bearing failure and recovery: technical and project management lessons learned (no. NASA/TP-2011-217116),2011
3. Bird-strike simulation for certification of the Boeing 787 composite moveable trailing edge;Composite Structures,2008
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