Cited by 35Space Exploration and TechnologyMineral Processing and GrindingMinerals Flotation and Separation Techniques

Evaluation of tribocharged electrostatic beneficiation of lunar simulant in lunar gravity

Open access
Quinn, Jacqueline W., Captain, Jim G., Weis, Kyle, Santiago-Maldonado, Edgardo, Trigwell, Steve·2013·Journal of Aerospace Engineering

Abstract

Tribocharged electrostatic beneficiation of a lunar simulant and actual Apollo regolith has been shown to be successful under a high lunar vacuum in which various degrees of efficient particle separation and mineral enrichment of up to a few hundred percent were achieved. In this paper, electrostatic beneficiation of a lunar simulant at 1/6g, as run on reduced gravity flights (RGFs), is reported. Enrichment of the target mineral ilmenite was achieved as high as 65 and 106% in the two RGF flights undertaken, showing that tribocharged electrostatic beneficiation is a viable process in the lunar environment. It was also shown that the efficiency of the separation was a factor in the orientation of the apparatus in the aircraft because the force of gravity was not perpendicular to the plane of the apparatus during the flight parabolas.

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Crossref · 10.1061/(asce)as.1943-5525.0000227

Cites

9 of 9 references verified0 citation errors · 0 not checkable

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  • In available literature, electrostatic separation is primarily investigated for enriching ilmenite from lunar regolith.

    “In the available literature, electrostatic separation is primarily investigated for enriching ilmenite from Lunar regolith [64,71,73-78].”

    From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [76]

    The Introduction describes electrostatic beneficiation of lunar simulants with the goal of enriching ilmenite, and the Conclusions report that the method enriched ilmenite. This supports the paper as an example of such research, but it does not establish that ilmenite enrichment is the primary focus of the available literature. (LLM, conf=0.82)

    Experimental — accuracy not yet measured
  • Three methods have been utilized for beneficiating lunar regolith through electrostatic forces: conductive induction via slide separators, tribocharging with parallel plate separators, and electrostatic traveling wave technique.

    “Besides, in the literature, three methods have been utilized for beneficiating Lunar regolith through the use of electrostatic forces: conductive induction via slide separators [71,73,74,79], tribocharging with parallel plate separators [70,75-78], and the electrostatic traveling wave technique [72,80-82].”

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Cites

Flagged first, then by citations

Research works printed but not linked: 9

  1. Cameron, E.N. (1992). "Apollo II Ilmenite Revisited". Space 92, The 3rd International Conference on Engineering, Construction, and Operations in Space. Denver, CO. WCSAR-TR- AR3-9201-3.
  2. Captain, J.G., Trigwell, S., Arens, E.E., Biris, A.S., Captain, J.E., Quinn, J.W., and Calle, c.r. (2007). "Tribocharging Lunar Simulant in Vacuum for Electrostatic Beneficiation", AlP Can! Proc., 880. STAfF 2007, Albuquerque, NM, 951-956.
  3. Heiken, G.H., Vaniman, D.T., and B.M. French, B.M. (Eds.). (1993). Lunar Source Book: A user's guide to the moon, UK: Cambridge University Press.
  4. Hintze, P.E., Curran, J., and Back, T. (2009). "Lunar Surface Stabilization via Sintering or the use of Heat Cured Polymers," Proc. 4i h AlAA Aerospace Sciences Meeting, Orlando, FL. AIAA 2009-1015
  5. Immer, C.D., Metzger, P.T., Nick, A., and Horan, R. (2011). "Apollo 12 lunar module exhaust plume impingement on lunar Surveyor III", Icarus, 211(2), 1089-1102.
  6. Metzger P.T., Li, X., Immer, C.D., and Lane, J. (2009). "ISRU implications of lunar and Martian plume effects", Proc. 4i h AlAA Aerospace Sciences Conference, Orlando, FL, AIAA 2009- 1204.
  7. Rao, D.E., Choudary, U. V., Erstfeld, T.E., Williams, R.J., and Chang, Y.A., (1979). "Extraction Processes for the Production of Aluminum, Titanium, Iron, Magnesium, and Oxygen from Nonterrestrial Materials". Space Resources and Space Settlements, NASA SP-428, pp. 257-274.
  8. Trigwell, S., Captain, J.G., Captain, J.E., Arens, E.E., Quinn, 1. W., and Calle, C.1. (2006). "Electrostatic Beneficiation of Lunar Simulant", Proc. ESA/IEJ/IEEE-IAS Joint Conference, UC Berkeley, CA, 297-306.
  9. Trigwell, S. (2002). "Correlation between Surface Structure and Tribocharging of Powders", PhD Dissertation, University of Arkansas at Little Rock, Little Roc, AR.

Cited by

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Authors
Quinn, J. W., Captain, J. G., Weis, K., Santiago-Maldonado, E., & Trigwell, S.
Affiliations
Kennedy Space Center (US)
Corresponding author
Trigwell, Steve
Venue
Journal of Aerospace Engineering
Published
2013-01
Volume
26
Issue
1
Pages
37-42
ISSN
  • 0893-1321 (ISSN-L)
  • 1943-5525
OpenAlex
W2022999328
Cited by
35
References
9
Citations by year
2026: 7 · 2025: 9 · 2024: 2 · 2023: 3 · 2022: 2 · 2021: 4 · 2020: 2 · 2019: 1 · 2018: 1 · 2016: 2 · 2014: 1 · 2013: 1
FWCI
2.14
Type
journal article
Language
en
Open access
Locations
  • Journal of Aerospace Engineering (publishedVersion)
  • NASA STI Repository (National Aeronautics and Space Administration) (submittedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Space Exploration and Technology
  • Physical Sciences › Engineering › Mechanical Engineering › Mineral Processing and Grinding
  • Physical Sciences › Environmental Science › Water Science and Technology › Minerals Flotation and Separation Techniques
Keywords
triboelectric charging, lunar regolith simulant, lunar gravity, particle separation, lunar resource utilization

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