Integration of ceramic matrix systems into coreless filament wound fiber-reinforced composite lightweight structures for lunar resource utilization

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES
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Abstract

Integrating ceramic matrix systems into coreless filament winding (CFW) enables the creation of sustainable, heat- and fire-resistant fiber composite lightweight structures. This study introduces a chemically bonded ceramic matrix system based on metakaolin, tailored for space applications utilizing lunar resources. The system employs acidic activation for processing with basalt/mineral fibers and alkaline activation for carbon fibers composites. Initially, the constituents of the matrix system are outlined, alongside potential synthesis pathways from lunar resources. Various formulations, incorporating different additives, are proposed. Through coupon compression testing, the most performative formulations for each activation type are selected for further investigation. The addition of zirconium silicate resulted in a higher compressive strength without significantly affecting the compressive modulus. The study then proceeds to experimentally characterize the matrix system’s viscosity. Subsequently, the processability of the proposed matrix system with CFW is demonstrated through the fabrication of generic medium-size lattice samples. Finally, these samples undergo destructive structural testing in compression. While emphasizing material development aspects, the investigation concludes that the feasibility of the proposed concept is validated through the successful fabrication and testing of generic CFW samples, affirming its potential use in space-related structural applications.

将陶瓷基质系统集成到无芯缠绕纤维增强复合轻质结构中,用于月球资源利用
将陶瓷基质系统集成到无芯长丝缠绕(CFW)中,可以制造出可持续、耐热和耐火的纤维复合轻质结构。本研究介绍了一种基于偏高岭土的化学键合陶瓷基质系统,该系统专为利用月球资源的太空应用而量身定制。该系统采用酸性活化法处理玄武岩/矿物纤维,采用碱性活化法处理碳纤维复合材料。首先,概述了基质系统的组成成分,以及利用月球资源的潜在合成途径。此外,还提出了包含不同添加剂的各种配方。通过试样压缩测试,为每种活化类型选择了性能最好的配方,以便进一步研究。添加硅酸锆可获得更高的抗压强度,而不会对压缩模量产生显著影响。研究接着对基质系统的粘度进行了实验表征。随后,通过制作一般的中等尺寸晶格样品,证明了带有 CFW 的拟议基质系统的可加工性。最后,对这些样品进行压缩破坏性结构测试。在强调材料开发方面的同时,调查得出结论,通过成功制作和测试通用 CFW 样品,验证了拟议概念的可行性,肯定了其在空间相关结构应用中的潜在用途。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
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