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评估行星际探测期间空间结构中胶粘剂接头的长期性能。

Assessing the Long-Term Performance of Adhesive Joints in Space Structures during Interplanetary Exploration.

作者信息

Charpentier Gabin, Lafont Ugo, Teixeira de Freitas Sofia

机构信息

Department of Aerospace Structures and Materials, Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft, The Netherlands.

ISAE ENSMA, Téléport 2, 1 Avenue Clément Ader, 86360 Chasseneuil-du-Poitou, France.

出版信息

Materials (Basel). 2023 Jul 13;16(14):4978. doi: 10.3390/ma16144978.

Abstract

Spacecraft experience minimal mechanical loads in space, but with the development of reusable spacecraft for interplanetary exploration and repeated landings, structures will be subjected to increased mechanical stress. The impact of the space environment on the aging of adhesive materials used in space structures over long-term applications is not well understood. This study investigates two commonly used adhesives in spacecraft assembly, namely Scotch-Weld™ EC-2216 and Scotch-Weld™ EC-9323-2, under two aging conditions: (1) high-energy electron irradiation using a Van de Graaf accelerator, and (2) thermal vacuum cycling. The research evaluates the evolution of intrinsic adhesive properties and adhesion to CFRP (carbon fiber-reinforced polymer) and aluminum adherents before and after exposure to these environmental conditions through tensile tests, peel tests, double-cantilever beam (DCB) tests, and dynamic mechanical analysis (DMA).

摘要

航天器在太空中承受的机械载荷极小,但随着用于星际探索和重复着陆的可重复使用航天器的发展,结构将承受更大的机械应力。长期应用中,太空环境对太空结构中使用的胶粘剂材料老化的影响尚不清楚。本研究在两种老化条件下研究了航天器组装中常用的两种胶粘剂,即Scotch-Weld™ EC-2216和Scotch-Weld™ EC-9323-2:(1)使用范德格拉夫加速器进行高能电子辐照,以及(2)热真空循环。该研究通过拉伸试验、剥离试验、双悬臂梁(DCB)试验和动态力学分析(DMA),评估了在暴露于这些环境条件之前和之后,胶粘剂固有性能的演变以及对碳纤维增强聚合物(CFRP)和铝粘附体的粘附力。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/b34f/10383705/41688ec709ed/materials-16-04978-g001.jpg

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