Cited by 45Planetary Science and ExplorationSpacecraft Design and TechnologyPhase Change Materials Research

Analysis of Solar-Heated Thermal Wadis to Support Extended-Duration Lunar Exploration

Balasubramaniam, R., Gokoglu, S., Sacksteder, K., Wegeng, R., Suzuki, N.·2011·Journal of Thermophysics and Heat Transfer

Abstract

The realization of the renewed exploration of the Moon presents many technical challenges; among them is the survival of lunar-surface assets during periods of darkness when the lunar environment is very cold. Thermal wadis are engineered sources of stored solar energy using modified lunar regolith as a thermal storage mass that can supply energy to protect lightweight robotic rovers or other assets during the lunar night. This paper describes an analysis of the performance of thermal wadis based on the known solar illumination of the Moon and estimates of producible thermal properties of modified lunar regolith. Analysis has been performed for the lunar equatorial region and for a potential outpost location near the Lunar South Pole. The calculations indicate that thermal wadis can provide the desired thermal energy and temperature control for the survival of rovers or other equipment during periods of darkness.

Integrity signals

Registry

Crossref · 10.2514/1.49843

Cites

15 of 15 references verified0 citation errors · 0 not checkable

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Claims the paper makes

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Claims other papers make about this one

Each is checked against this paper’s own text: does it say what the citing paper says it does?

  • The use of solar energy to sinter and/or melt lunar regolith can coalesce it into a continuous block with higher thermal conductivity than the natural lunar regolith.

    “The use of solar energy to sinter and/or melt lunar regolith can be a way to coalesce it into a continuous block with higher thermal conductivity than the natural lunar regolith. 184,185”
  • The power generation of the Stirling generator will not be more than 70 kW.

    “However, the power generation of the Stirling generator will not be more than 70 kW. 184”

Cites

Flagged first, then by citations

Research works printed but not linked: 3

  1. Balasubramaniam R., 2009, 47th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper
  2. Colozza A. J., 1991, NASA CR, 189073
  3. Wesselink A. J., 1948, Bulletin of the Astronomical Institutes of The Netherlands, 10, 351

Cited by

Sorted by citations

Authors
Balasubramaniam, R., Gokoglu, S., Sacksteder, K., Wegeng, R., & Suzuki, N.
Affiliations
  • Glenn Research Center (US)
  • NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
  • Pacific Northwest National Laboratory (US)
  • National Aeronautics and Space Administration (US)
Venue
Journal of Thermophysics and Heat Transfer
Published
2011-01
Volume
25
Issue
1
Pages
130-139
ISSN
  • 0887-8722 (ISSN-L)
  • 1533-6808
OpenAlex
W1977676790
Cited by
45
References
15
Citations by year
2026: 5 · 2025: 4 · 2024: 2 · 2023: 4 · 2022: 4 · 2021: 2 · 2019: 2 · 2016: 1 · 2015: 2 · 2014: 4 · 2013: 5 · 2012: 5
FWCI
2.89
Type
journal article
Language
en
Open access
closed
Locations
  • Journal of Thermophysics and Heat Transfer (publishedVersion)
  • NASA STI Repository (National Aeronautics and Space Administration) (submittedVersion)
  • NASA Technical Reports Server (NASA) (submittedVersion)
Topics
  • Physical Sciences › Earth and Planetary Sciences › Space and Planetary Science › Planetary Science and Exploration
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
  • Physical Sciences › Engineering › Mechanical Engineering › Phase Change Materials Research
Keywords
lunar rover, thermal mass, solar energy storage, thermal analysis

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