Ground and parabolic flight testing of a magnetic and electrostatic separation system for lunar regolith beneficiation

IF 3.7 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE
Blake A. Coffman, Jacob N. Ortega, Peter Bachle, Jeffrey Smith, Fateme Rezaei, David Bayless, William Schonberg, Kirby Runyon, Frank D. Han
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引用次数: 0

Abstract

We present an end-to-end design, build, and testing, of a regolith beneficiation system under both Earth gravity and simulated lunar gravity. The system combines a dual-stage magnetic separator followed by an electrostatic sieve to enrich high-value minerals from bulk lunar regolith simulant, targeting plagioclase feldspar which spans the solid-solution series between anorthite and albite. The magnetic separator consists of a dual-strength set of N-52 and N-42 neodymium permanent magnets to sort the simulant particles based on their magnetic susceptibility. The downstream electrostatic sieve separates particles by size using a single-phase 50% duty-cycle wave with a peak voltage between 3.0 kV and 6.0 kV and operating frequencies ranging from 15 Hz to 30 Hz. The combined system produces four output streams: concentrated iron particulates, bulk basalt, and two sized anorthite fractions according to a target particle size range. The design objective was to obtain an anorthite-rich feedstock exceeding 70 wt% within a 20μm to 200μm size range. A prototype unit was first designed, built, and tested under Earth gravity to prove the concept. Then an adapted unit was built and tested under simulated lunar gravity through parabolic flights. Experiments using multiple lunar regolith simulants under both Earth and reduced-gravity conditions demonstrate consistent mineral and size separation, with improved performance observed under lunar gravity. X-ray Diffraction (XRD) with Rietveld refinement confirmed the success of the reduced-gravity separation: for the L2W60-g814 Mare simulant, plagioclase increased from 35.5 wt% in the feed to 70.6 wt% in the recovered product, approximately doubling its concentration and meeting the system design objective. Pyroxene and olivine, initially present in the feed, were not detected above the approximate XRD detection limit in the reduced-gravity product. These results demonstrate that combined magnetic and electrostatic beneficiation can successfully produce a concentrated plagioclase-rich feedstock under lunar-relevant gravity conditions, supporting its use as a front-end process for lunar in-situ resource utilization (ISRU) such as downstream aluminum and oxygen extraction and additive manufacturing.
月球风化层选矿磁静电分离系统的地面和抛物线飞行试验
我们提出了一个端到端的设计,构建和测试,在地球重力和模拟月球重力下的风化层选矿系统。该系统结合双级磁选机和静电筛,从模拟月球风化层中富集高价值矿物,目标是斜长石长石,该长石横跨钙长石和钠长石之间的固溶系列。该磁选机由一组双重强度的N-52和N-42钕永磁体组成,用于根据磁化率对模拟颗粒进行分选。下游静电筛采用峰值电压为3.0 kV ~ 6.0 kV,工作频率为15 Hz ~ 30 Hz的单相50%占空比波,按粒度对颗粒进行分离。该组合系统产生四种输出流:浓缩铁颗粒、大块玄武岩和根据目标粒度范围划分的两种钙长石馏分。设计目标是在20μm到200μm的尺寸范围内获得超过70% wt%的富钙长石原料。首先设计、制造了一个原型装置,并在地球重力下进行了测试,以证明这一概念。然后建造了一个改装单元,并通过抛物线飞行在模拟月球重力下进行了测试。在地球和失重条件下使用多个月球风化模拟物进行的实验表明,矿物和粒度分离的一致性,在月球重力条件下观察到的性能有所改善。采用Rietveld细化的x射线衍射(XRD)证实了减轻重力分离的成功:对于L2W60-g814 Mare模拟物,斜长石在进料中的含量从35.5%增加到回收产品中的70.6 %,大约增加了一倍,达到了系统设计目标。最初存在于进料中的辉石和橄榄石,在还原产物中未检测到超过近似XRD检测限。这些结果表明,在与月球相关的重力条件下,磁性和静电联合选矿可以成功地生产出富含斜长石的浓缩原料,支持其作为月球原位资源利用(ISRU)的前端工艺,如下游的铝和氧提取以及增材制造。
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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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