2010
DOI: 10.1061/(asce)as.1943-5525.0000026
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Geotechnical Properties of NT-LHT-2M Lunar Highland Simulant

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Cited by 45 publications
(15 citation statements)
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“…FJS-1 has a cohesion of 8 kPa although it is not stated at which density 23 , however, studies have investigated the slope angle and self-standing heights 24,25 . There are no published data on the cohesion of DNA or NU-LHT-3M, but it is considered to be negligible in NU-LHT-2M 26 . In this study cohesion was measured by lowering a plastic plate into a box filled with EAC-1A.…”
Section: Cohesionmentioning
confidence: 99%
“…FJS-1 has a cohesion of 8 kPa although it is not stated at which density 23 , however, studies have investigated the slope angle and self-standing heights 24,25 . There are no published data on the cohesion of DNA or NU-LHT-3M, but it is considered to be negligible in NU-LHT-2M 26 . In this study cohesion was measured by lowering a plastic plate into a box filled with EAC-1A.…”
Section: Cohesionmentioning
confidence: 99%
“…An OHAUS Discovery DV215CD precision balance with a readability of 0.01 mg was placed inside the glovebox to measure the mass gain of the sample during adsorption. A thin layer of NU-LHT-2M in its standard particle size distribution (Zeng et al 2010) was spread over a stainless steel petri dish with 75 mm diameter and baked-out at >100 °C for 4 h under continuous vacuum pumping and a pressure of approximately 10 -1 mbar. The sample was then transferred into the humidity-controlled volume of the glovebox and left there for at least 12 h and up to 48 h to adsorb water from the glovebox atmosphere at 1 % relative humidity.…”
Section: Sample Hydrationmentioning
confidence: 99%
“…However, JSC-1 or Johnson Space Center Number One A (JSC-1A) simulants are insufficient for large-scale simulation programs due to their scarce quantities. New lunar regolith simulants with large procurement, such as NASA/USGS-Lunar Highlands Type-2 Medium regolith simulant (NU-LHT-2M) (Stoeser et al 2010;Zeng et al 2010), are thus currently being actively used in large-scale lunar programs (e.g., ESA PROSPECT).…”
Section: Scanning Electron Microscope Analysis Of Particle Characterimentioning
confidence: 99%