Research on the Encapsulation Device for Lunar Samples

The encapsulation of lunar samples is a core research area in the third phase of the Chinese Lunar Exploration Program.The seal assembly,opening and closing mechanism(OCM),and locking mechanism are the core components of the encapsulation device of the lunar samples,and the requirements of a tight seal,lightweight,and low power make the design of these core components difficult.In this study,a combined sealing assembly,OCM,and locking mechanism were investigated for the device.The sealing architecture consists of rubber and an Ag-In alloy,and a theory was built to analyze the seal.Experiments of the electroplate Au coating on the knife-edge revealed that the hermetic seal can be significantly improved.The driving principle for coaxial double-helical pairs was investigated and used to design the OCM.Moreover,a locking mechanism was created using an electric initiating explosive device with orifice damping.By optimizing the design,the output parameters were adjusted to meet the requirements of the lunar explorer.The experimental results showed that the helium leak rate of the test pieces were not more than 5×10^(-11) Pa·m^(3)·s^(-1),the minimum power of the OCM was 0.3 W,and the total weight of the principle prototype was 2.9 kg.The explosive driven locking mechanism has low impact.This investigation solved the difficulties in achieving tight seal,light weight,and low power for the lunar explorer,and the results can also be used to explore other extraterrestrial objects in the future.

Experimental constraints on the formation of oxychlorine species by UV irradiation and mechanical pulverization on the lunar surface

Perchlorate and chlorate are present in various extraterrestrial celestial bodies throughout the solar system,such as Mars,the moon,and asteroids.To date,the origin mechanisms of perchlorate and chlorate on the Martian surface have been well-established;however,relatively little attention has been cast to airless bodies.Here,we experimentally investigated the potential oxidation mechanisms of chloride to chlorate and perchlorate,such as ultraviolet irradiation under H_(2)O-and O_(2)-free conditions and mechanical pulverization processes.Individual minerals,olivine,pyroxene,ilmenite,magnetite,TiO_(2)and anhydrous ferric sulfate,and lunar regolith simulants(low Ti,CLRS-1;high-Ti,CLRS-2)and their metallic iron(Fe^( 0))bearing counterparts were examined.We found that pulverization of dry matrix material-halite mixtures,even in the presence of O_(2),does not necessarily lead to perchlorate and chlorate formation without involving water.Under photocatalytic and H_(2)O and O_(2)-free conditions,olivine and pyroxene can produce oxychlorine(ClO_(x)^(−))species,although the yields were orders of magnitude lower than those under Martian-relevant conditions.Nanophase-Fe^(0)particles in the lunar regolith and the common photocatalyst TiO_(2)can facilitate the ClO_(x)^(−)formation,but their yields were lower than those with olivine.The oxides ilmenite and magnetite did not efficiently contribute to ClO_(x)^(−)production.Our results highlight the critical role of H_(2)O in the oxidation chloride to chlorate and perchlorate,and provide essential insights into the environmental influence on the formation of oxychlorine species on different celestial bodies.

Metallurgical performance evaluation of space-weathered Chang’e-5 lunar soil

Space metallurgy is an interdisciplinary field that combines planetary space science and metallurgical engineering.It involves systematic and theoretical engineering technology for utilizing planetary resources in situ.However,space metallurgy on the Moon is challenging because the lunar surface has experienced space weathering due to the lack of atmosphere and magnetic field,making the mi-crostructure of lunar soil differ from that of minerals on the Earth.In this study,scanning electron microscopy and transmission electron microscopy analyses were performed on Chang’e-5 powder lunar soil samples.The microstructural characteristics of the lunar soil may drastically change its metallurgical performance.The main special structure of lunar soil minerals include the nanophase iron formed by the impact of micrometeorites,the amorphous layer caused by solar wind injection,and radiation tracks modified by high-energy particle rays inside mineral crystals.The nanophase iron presents a wide distribution,which may have a great impact on the electromagnetic prop-erties of lunar soil.Hydrogen ions injected by solar wind may promote the hydrogen reduction process.The widely distributed amorph-ous layer and impact glass can promote the melting and diffusion process of lunar soil.Therefore,although high-energy events on the lun-ar surface transform the lunar soil,they also increase the chemical activity of the lunar soil.This is a property that earth samples and tradi-tional simulated lunar soil lack.The application of space metallurgy requires comprehensive consideration of the unique physical and chemical properties of lunar soil.

Fast solution to the free return orbit's reachable domain of the manned lunar mission by deep neural network

It is important to calculate the reachable domain(RD)of the manned lunar mission to evaluate whether a lunar landing site could be reached by the spacecraft. In this paper, the RD of free return orbits is quickly evaluated and calculated via the classification and regression neural networks. An efficient databasegeneration method is developed for obtaining eight types of free return orbits and then the RD is defined by the orbit’s inclination and right ascension of ascending node(RAAN) at the perilune. A classify neural network and a regression network are trained respectively. The former is built for classifying the type of the RD, and the latter is built for calculating the inclination and RAAN of the RD. The simulation results show that two neural networks are well trained. The classification model has an accuracy of more than 99% and the mean square error of the regression model is less than 0.01°on the test set. Moreover, a serial strategy is proposed to combine the two surrogate models and a recognition tool is built to evaluate whether a lunar site could be reached. The proposed deep learning method shows the superiority in computation efficiency compared with the traditional double two-body model.

Enhancing the vertical resolution of lunar penetrating radar data using predictive deconvolution

The Yutu-2 rover onboard the Chang’E-4 mission performed the first lunar penetrating radar detection on the farside of the Moon.The high-frequency channel presented us with many unprecedented details of the subsurface structures within a depth of approximately 50 m.However,it was still difficult to identify finer layers from the cluttered reflections and scattering waves.We applied deconvolution to improve the vertical resolution of the radar profile by extending the limited bandwidth associated with the emissive radar pulse.To overcome the challenges arising from the mixed-phase wavelets and the problematic amplification of noise,we performed predictive deconvolution to remove the minimum-phase components from the Chang’E-4 dataset,followed by a comprehensive phase rotation to rectify phase anomalies in the radar image.Subsequently,we implemented irreversible migration filtering to mitigate the noise and diminutive clutter echoes amplified by deconvolution.The processed data showed evident enhancement of the vertical resolution with a widened bandwidth in the frequency domain and better signal clarity in the time domain,providing us with more undisputed details of subsurface structures near the Chang’E-4 landing site.

Damage constitutive model of lunar soil simulant geopolymer under impact loading

Lunar base construction is a crucial component of the lunar exploration program,and considering the dynamic characteristics of lunar soil is important for moon construction.Therefore,investigating the dynamic properties of lunar soil by establishing a constitutive relationship is critical for providing a theoretical basis for its damage evolution.In this paper,a split Hopkinson pressure bar(SHPB)device was used to perform three sets of impact tests under different pressures on a lunar soil simulant geopolymer(LSSG)with sodium silicate(Na_(2)SiO_(3))contents of 1%,3%,5%and 7%.The dynamic stressestrain curves,failure modes,and energy variation rules of LSSG under different pressures were obtained.The equation was modified based on the ZWT viscoelastic constitutive model and was combined with the damage variable.The damage element obeys the Weibull distribution and the constitutive equation that can describe the mechanical properties of LSSG under dynamic loading was obtained.The results demonstrate that the dynamic compressive strength of LSSG has a marked strain-rate strengthening effect.Na_(2)SiO_(3) has both strengthening and deterioration effects on the dynamic compressive strength of LSSG.As Na_(2)SiO_(3) grows,the dynamic compressive strength of LSSG first increases and then decreases.At a fixed air pressure,5%Na_(2)SiO_(3) had the largest dynamic compressive strength,the largest incident energy,the smallest absorbed energy,and the lightest damage.The ZWT equation was modified according to the stress response properties of LSSG and the range of the SHPB strain rate to obtain the constitutive equation of the LSSG,and the model’s correctness was confirmed.

Fundamental Study on Response Properties of Structures Constructed on Lunar Regolith

The Artemis Program, for constructing the lunar base, is in progress. How to design and construct architectural and civil engineering structures in the lunar environment has become an important issue. The lunar surface is covered with soft sand, called regolith, and it is required to protect lunar bases and structures, as well as internal precision equipment, against vibrational disturbances such as moonquakes and meteorite collisions. Therefore, in this study, the static and cyclic triaxial compression tests of the regolith simulant were conducted. The reference strain and equivalent damping factor of the regolith simulant were smaller compared to sandy soil on Earth. In addition, a shaking table test using model specimens was conducted on the response properties of regolith ground alone and structures set on regolith ground. The buried foundation and pile foundation notably suppressed the horizontal response attributed to the rocking component compared to a direct foundation.

利用Lunar Prospector Doppler数据解算并分析月球重力场

Doppler技术可高精度测定卫星之间的距离变化率,可以和其他技术联合用于月球卫星定轨。本文利用Lunar Prospector月球项目4个月的Doppler跟踪数据,解算了75阶次月球重力场模型。首先介绍了数据预处理方法、力模型的使用及参数设置等关键技术,然后把解算的重力场模型与同阶次的其他月球重力场模型进行比较,可以看出低阶位系数较LP75G月球重力场模型稍差,但高阶位系数精度有所提高,可能是仅利用了低轨单星数据的原因。

月球表面岩石类型的分布特征：基于Lunar Prospector (LP)伽马射线谱仪探测数据的反演

Apollo和LP伽马射线谱仪获取了全月10种元素的分布图,通过已有的月岩以及陨石的化学成分数据,将伽马射线谱仪探测数据与这些数据融合,用Th-Fe-Mg三角图解定性的获得元素含量与岩石类型的相关性,同时通过以前融合的数据,获得了月海玄武岩、月陆斜长岩、KREEP岩和富镁岩的全月球表面岩石类型分布图。

GE Lunar Prodigy双能X射线骨密度仪故障维修3例

介绍了GE Lunar Prodigy双能X射线骨密度仪的工作原理,分析了GE Lunar Prodigy双能X射线骨密度仪3例典型故障的原因及排除过程,并提出了预防性维护建议,为临床工程师排除相似故障提供了参考。

月球样品的中子活化分析技术研究

月球的起源是月球研究的核心问题。月球探测任务返回的数据和样品极大地提高了人类对地月系统的认知,同时也发现了更多未解之谜,亟待未来的探测任务和科学研究来解答。嫦娥五号月壤是我国首次地外天体采集返回的样品,也是继美国和苏联探月采样任务45年后人类再次获得的月球样品。鉴于月球样品的珍贵性和特殊性,利用先进技术开展其全元素含量的非破坏精准分析对于认识月球演化和月球资源就地开发利用具有重要的意义。依托大型核反应研究堆和加速器中子注量率优势,利用中子活化分析技术可实现月球样品中的全元素非破坏分析:1)仪器中子活化分析技术(INAA)可测量Na—U元素之间的60余种元素;2)瞬发γ中子活化分析技术(PGNAA)可补充测量INAA不适合测量的元素如H、B、C、N等;3)中子深度剖面分析技术(NDP)可测量样品近表面(微米级)聚变能源3He的浓度深度分布;4)缓发中子测量技术(DNC)可定量样品中痕量裂变核素如^(235)U和^(239)Pu,并结合INAA可测量238U/235U同位素比值;5)14 MeV快中子活化分析技术(FNAA)可测量INAA和PGNAA不灵敏或不适合测量的元素如O、Si、P等。因此,中子活化分析技术(NAA)可有效解决月球样品中全元素、非破坏和精准测量问题,为我国深空探测珍贵样品研究提供核分析技术支撑。

Selection and thermal physical characteristics analysis of in-situ condition preserved coring lunar rock simulant in extreme environment

With the increasing scarcity of Earth’s resources and the development of space science and technology,the exploration, development, and utilization of deep space-specific material resources(minerals, water ice, volatile compounds, etc.) are not only important to supplement the resources and reserves on Earth but also provide a material foundation for establishing extraterrestrial research bases. To achieve large depth in-situ condition-preserved coring(ICP-Coring) in the extreme lunar environment, first, lunar rock simulant was selected(SZU-1), which has a material composition, element distribution, and physical and mechanical properties that are approximately equivalent to those of lunar mare basalt. Second, the influence of the lunar-based in-situ environment on the phase, microstructure, and thermal physical properties(specific heat capacity, thermal conductivity, thermal diffusivity, and thermal expansion coefficient)of SZU-1 was explored and compared with the measured lunar rock data. It was found that in an air atmosphere, low temperature has a more pronounced effect on the relative content of olivine than other temperatures, while in a vacuum atmosphere, the relative contents of olivine and anorthite are significantly affected only at temperatures of approximately-20 and 200 ℃. When the vacuum level is less than100 Pa, the contribution of air conduction can be almost neglected, whereas it becomes dominant above this threshold. Additionally, as the testing temperature increases, the surface of SZU-1 exhibits increased microcracking, fracture opening, and unevenness, while the specific heat capacity, thermal conductivity,and thermal expansion coefficient show nonlinear increases. Conversely, the thermal diffusivity exhibits a nonlinear decreasing trend. The relationship between thermal conductivity, thermal diffusivity, and temperature can be effectively described by an exponential function(R^(2)>0.98). The research results are consistent with previous studies on real lunar rocks. These research findings are expected to be applied in the development of the test and analysis systems of ICP-Coring in a lunar environment and the exploration of the mechanism of machine-rock interaction in the in-situ drilling and coring process.

月球资源开发利用的进展与展望

中国探月工程“绕、落、回”三步走圆满收官,后续将建立国际月球科研站,并进一步规划建立月球基地。月球探测任务由探测勘察进入到开发利用新阶段,月面资源的勘查、开发和利用是未来月球探测的重点任务。总结了月球资源开发利用方面的国内外重要进展,涉及月球资源勘探、水冰等挥发分分析、月球矿物冶炼与材料制备、月面建造与月壤3D打印等四个方面。同时,月球资源开发利用面临极端月面环境、独特月壤理化特性、全流程无人自主控制等重大挑战,为解决这些问题,提出了未来月球资源开发利用的重点任务和研究思路,可为后续科学研究和工程任务实施提供参考。

离散元法在月面建造力学分析中的研究及应用

【目的】为了深入了解月面建造过程中月壤的力学特性,评估月基装备性能,优化月面建造作业,开展离散元法(discrete element method,DEM)在月壤接触力学领域的应用调查研究,旨在利用离散元法为未来月球基地建设提供理论指导和技术支持。【研究现状】基于地质勘探、资源采集及运输、建造作业等月面原位建造任务场景,分析月壤颗粒的建模与参数标定,介绍月基装备与月壤的接触作用研究现状,概述离散元法在钻-壤作用模拟、铲-壤作用模拟、轮-壤作用模拟及足-壤作用模拟中的应用,探讨基于离散元法的天然月基承载力分析。【结论与展望】提出降低几何模型复杂度、优化粒间接触模型及参数是提高宏观尺度月壤离散元建模精度以应对大规模月面建造场景的有效方法。认为利用离散元法进行铲挖式月壤采集装置及足式月球车设计在未来可以为月面建造提供可靠的技术支持。面向月面建造,离散元法将在水冰资源利用、建筑物月面承载力分析等方面提供科学依据。

月球空间天气探测与研究进展

稳定的天体地质构造、与地球合适的距离、无稠密大气和全球磁场,使得月球成为日地月空间天气监测和研究的天然优良实验室。回顾了国内外月球空间天气探测和研究进展,梳理了月球空间天气关键科学问题及预报应用问题,提出了建立月球空间天气监测站的构想,明确了监测站具体科学目标,并介绍了监测站三大系统构成及相互关系,包括监测系统、科学研究系统以及建模与预报系统。建立月球空间天气监测站对研究太阳爆发活动、日地月耦合关系以及月球局地环境的变化具有重要的科学意义,也有利于促进月球空间天气建模和预报技术的发展,提升未来月球科研探索任务空间环境保障能力。

月面原位水资源获取技术与发展趋势

随着深空探测活动的持续推进,月球探测已成为开展行星际探测的重要部分.月球原位资源利用是保障载人月球探测及月面长期驻留的关键技术途径,中国已将月面原位水获取方法列为月球探测的关键技术之一.月面原位水获取方法主要分为极区水冰勘探开采和月壤氢还原制水两种技术途径.现有勘探到的水冰资源主要位于月球极区,分布不均匀,开采难度大.目前研究提出了多种不同类型的极区水冰勘探开采方法,但实际效果有待月面原位试验验证.月壤加氢还原制水技术方法工作条件不受区域限制,应用范围较广,但仍存在反应条件要求高、能耗大等技术限制,未来需在节能和有效矿物成分富集等方面有所突破.

月球探测器鲁棒环形山检测及光学导航方法

针对月球探测器环形山检测方法受光照影响、鲁棒性差的问题,本文提出一种基于极大熵阈值三值化的鲁棒环形山检测算法。采用不同滤波核对图像进行去噪平滑,然后对处理后的图像进行极大熵阈值分割、将图像信息三值化,去除图像对光源的敏感性,同时最大程度保留图像信息;提出一种归一化多指标约束环形山匹配和拟合方法完成环形山提取,将环形山提取算法应用于光学导航中进行打靶实验验证算法实时性表现。仿真结果表明:与传统基于形态学或自适应边缘检测的方法相比,本文方法在较大尺度条件下提取出连续、光滑的环形山边缘,有效环形山数量提升35%以上,同时实时性更好、计算消耗降低40%;基于鲁棒环形山提取的光学导航算法实时性更好。

Simulation Research on the Effect of Spreading Process Parameters on the Quality of Lunar Regolith Powder Bed in Additive Manufacturing

Lunar surface additive manufacturing with lunar regolith is a key step in in-situ resource utilization.The powder spreading process is the key process,which has a major impact on the quality of the powder bed and the precision of molded parts.In this study,the discrete element method(DEM)was adopted to simulate the powder spreading process with a roller.The three powder bed quality indicators,including the molding layer offset,voidage fraction,and surface roughness,were established.Besides,the influence of the three process parameters,which are roller’s translational speed,rotational speed,and powder spreading layer thickness on the powder bed quality indicators was also analyzed.The results show that with the reduction of the powder spreading layer thickness and the increase of the rotational speed,the offset increased significantly;when the translational speed increased,the offset first increased and then decreased,which resulted in an extreme value;with the increase of the layer thickness and the decrease of the translational speed,the values for voidage fraction and surface roughness significantly reduced.The powder bed quality indicators were adopted as the optimization objective,and the multi-objective parameter optimization was carried out.The predicted optimal powder spreading parameters and powder bed quality indicators were then obtained.Moreover,the optimal values were then verified.This study can provide informative guidance for in-situ manufacturing at the moon in future deep space exploration missions.

冰晶石-月壤熔盐体系初晶温度的研究

冰晶石熔盐电解法可实现月壤原位利用制备金属和氧气,研究冰晶石-月壤熔盐体系的初晶温度对电解槽稳定运行具有重要意义。本文以火山渣和玄武岩复配的NEU-1月壤仿真样为原料,与冰晶石、CaF_(2)混合配置电解质,将其作为待测试样,利用差热分析法测量了不同月壤仿真样添加量、不同分子比的冰晶石熔盐体系的初晶温度。结果表明,当分子比为2.2时,随着月壤仿真样添加量从0%增加至24%,冰晶石熔盐体系的初晶温度从974.9℃降低至932.0℃;每添加1%的月壤仿真样,冰晶石熔盐体系的初晶温度降低约1.79℃;当月壤仿真样添加量为8%时,随着分子比从2.2升高至2.7,冰晶石熔盐体系的初晶温度从960.0℃升高至979.4℃。

ESA月球村建造计划解析及启示

月球基地在未来具有重要的战略价值,可作为空间安全基地以及航天科学研究的平台。欧洲航天局(ESA)于2015年提出月球村的概念,并于2020年由其并行设施中心(CDF)发表了研究报告《月球村:月球栖息地概念设计》。本文基于该研究报告,首先,介绍了月球村的基本概念,包括其系统划分和总体布局,概述了月球村计划以建造月球栖息地为主要任务的具体实现方案。随后,本文解析了月球村计划的核心——月球栖息地的内部建筑设计与功能分区,并对月球栖息地刚性支撑框架+柔性充气外壳的混合结构特点进行了详细说明。最后,本文从电力、热控、辐射屏蔽三个角度分析了月球栖息地的维保系统设计,为未来的月球基地建造方案和计划提供参考。