Facing compositional heterogeneity and thermal cycling challenges in lunar regolith based geopolymer for sustainable extraterrestrial construction

IF 3.4 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE
Zihan Zhou , Shuo Li , Guo Hu , Jun Wu , Chuanqin Yao , Fujun Niu , Jinbo Chen
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Abstract

This study developed a high-fidelity lunar regolith simulant (GCD-2) that matched the physicochemical characteristics of Chang'e−6 real lunar samples. Then, a dry mixture of GCD-2 (acting as a precursor) and solid sodium silicate (acting as an activator) was used to synthesize the Lunar regolith based geopolymer (LRG) via the one-part method with the addition of water. An environmental-compositional framework was established to elucidate the coupling effects of extreme lunar temperature cycling (−178 °C–113 °C, 700 h/cycle) and elemental ratios (Ca/Si and Al/Si) in precursor on the mechanical properties of LRG. Multiscale characterization techniques, including Scanning Electron Microscopy-Energy Dispersive X-ray Spectroscopy, X-ray Diffraction, Thermogravimetric Analysis, and Nitrogen Adsorption-Desorption measurements, were integrated with analysis methodologies (Brunauer-Emmett-Teller, Barrett-Joyner-Halenda, Density Functional Theory) to examine microstructural evolution. Results demonstrated that increasing Ca/Si ratio (from 0.26 to 0.35) enhanced the compressive strength of the LRG but exacerbated cryogenic susceptibility compared to the baseline group (Ca/Si = 0.26 and Al/Si = 0.34). Conversely, increasing Al/Si ratio (from 0.34 to 0.58) initially improved the compressive strength and reduced cryogenic susceptibility, followed by a decline in mechanical properties and an increase in cryogenic susceptibility. The LRG with Ca/Si of 0.35 and Al/Si of 0.58 achieved the maximum compressive strength (52.25 MPa), along with superior post-cryogenic strength retention. An optimized operational period for mixing and casting of the LRG at lunar surface was suggested to be within 100 h before high-temperature phase of the lunar day. Furthermore, cryogenic degradation in the LRG with high-Ca system was determined by the coupled internal and external factors, whereas the degradation in the low-Ca systems was predominantly affected by the external factor. The internal effect involved the collapse of the gel network, propagating the degradation of the pore structure, while the external effect included pore water freezing-induced cryo-suction and gel phase incompatibility, which governed detrimental pore evolution. The results of the current study can provide theoretical foundation for optimizing lunar construction method, advancing cost-effective and sustainable extraterrestrial habitat engineering.
面向可持续地外建筑的月壤基地聚合物的成分非均质性和热循环挑战
本研究开发了一种高保真的月球风化模拟物(GCD-2),该模拟物与嫦娥6号真实月球样品的物理化学特征相匹配。然后,以GCD-2(作为前驱体)和固体硅酸钠(作为活化剂)的干燥混合物为原料,加水,采用一组份法合成月球风化土基地聚合物(LRG)。建立了一个环境-成分框架,阐明了极端月球温度循环(- 178°C - 113°C, 700 h/循环)和前驱体元素比(Ca/Si和Al/Si)对LRG力学性能的耦合影响。多尺度表征技术,包括扫描电子显微镜-能量色散x射线光谱学,x射线衍射,热重分析和氮吸附-解吸测量,与分析方法(Brunauer-Emmett-Teller, Barrett-Joyner-Halenda,密度泛函数理论)相结合,以检查微观结构的演变。结果表明,与基线组(Ca/Si = 0.26和Al/Si = 0.34)相比,Ca/Si比值的增加(从0.26增加到0.35)增强了LRG的抗压强度,但加剧了低温敏感性。相反,当Al/Si比值从0.34增加到0.58时,材料的抗压强度提高,低温敏感性降低,随后力学性能下降,低温敏感性增加。Ca/Si为0.35、Al/Si为0.58时,LRG的抗压强度最大(52.25 MPa),低温后强度保持良好。建议在月球表面进行LRG混合和铸造的最佳操作周期为在月球日高温阶段前100 h内。此外,高钙体系下LRG的低温降解是由内外因素耦合决定的,而低钙体系下LRG的低温降解主要受外部因素的影响。内部影响包括凝胶网络的崩溃,传播孔隙结构的退化,而外部影响包括孔隙水冻结引起的低温吸力和凝胶相不相容,这控制了有害的孔隙演化。研究结果可为优化月球建设方法,推进经济高效、可持续的地外栖息地工程提供理论依据。
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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