Design and Analysis of a Novel Membrane Deployable Solar Array Based on STACER Deployable Mechanism for CubeSats

Author:

Tingrui Li,Kaijie DongORCID,Tianyu Zhou,Duanling LiORCID

Publisher

Springer Nature Singapore

Reference16 articles.

1. Li, B.: Mechanical Characteristics Analysis of Tensioned Membrane Structure and Design of Triangular Prism Membrane Support Mast. Harbin Institute of Technology, Harbin China (2021). (in Chinese)

2. Ren, S., et al.: Overview of solar wing for CubeSat. Spacecraft Eng. 24(2), 109–118 (2015). (in Chinese)

3. Hou, Y.: The Design and Application of Deployable Solar Array. Beijing University of Posts and Telecommunications, Beijing, China (2020). (in Chinese)

4. Sawada, H., et al.: Mission report on the solar power sail deployment demonstration of IKAROS. In: 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 19th AIAA/ASME/AHS Adaptive Structures Conference 13t. (2011)

5. Mansell, J., et al.: Orbit and attitude performance of the LightSail 2 solar sail spacecraft. In: AIAA Scitech 2020 Forum (2020)

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