G. Zanotti, I. Troisi, A. Dottori, M. R. Lavagna | 2024 | Aerospace
DOI 10.3390/aerospace11040295Review state
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This paper presents the characterization of the lunar simulant NU-LHT-2M, focusing on its properties relevant to oxygen extraction via low-temperature carbothermal reduction. The study outlines methods for simulant characterization, including composition, physical, mechanical, and thermal properties, and discusses their importance for in situ resource utilization (ISRU) on the Moon. This paper characterizes the lunar simulant NU-LHT-2M for oxygen/water extraction via carbothermal reduction. It outlines tests for composition, physical/mechanical properties, solid-fluid interaction, and thermal behavior. Results are compared with bibliographic data, and implications for ISRU technologies and lunar plant design are discussed. The paper discusses the characterization of the NU-LHT-2M lunar simulant for oxygen extraction via carbothermal reduction. It provides an overview of lunar regolith composition, including mineral types and their abundances, and compares them with the simulant. The study focuses on simulant testing and its relevance to lunar resource utilization. The paper discusses lunar regolith composition, mineral modal proportions, and the need for simulants to replicate luna
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Composition tests
characterization
Physical and mechanical tests
characterization
Solid fluid interaction
characterization
Thermal tests
characterization
Inductively coupled plasma Optical emission spectrometry technique (ICP-OES)
composition
Sieving
granulometry
SEM
grains shape, agglomeration status
Helium pycnometer
density of the grains/Specific gravity
density
not specified
granulometry distribution
not specified
particle shape
not specified
compressibility
not specified
shear properties
not specified
penetration resistance
not specified
moisture content
not specified
optical properties
not specified