Earth and Space 2021 2021
DOI: 10.1061/9780784483374.106
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Requirements Development Framework for Lunar In Situ Surface Construction of Infrastructure

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Cited by 4 publications
(6 citation statements)
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“…In the following, the energy consumption of two alternative blast shield construction methods are calculated and compared to the energy consumption of the proposed method. We note that the creation of un-cast regolith berms, as proposed by Mueller et al (2009) and Moses and Mueller (2021), is not discussed here. This method probably would need less energy than the other construction methods, but comes with other disadvantages: the impacting stream of spacecraft exhaust and pebbles/dust could erode a regolith berm over time (Morris, 2012).…”
Section: Comparison To Other Construction Methodsmentioning
confidence: 98%
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“…In the following, the energy consumption of two alternative blast shield construction methods are calculated and compared to the energy consumption of the proposed method. We note that the creation of un-cast regolith berms, as proposed by Mueller et al (2009) and Moses and Mueller (2021), is not discussed here. This method probably would need less energy than the other construction methods, but comes with other disadvantages: the impacting stream of spacecraft exhaust and pebbles/dust could erode a regolith berm over time (Morris, 2012).…”
Section: Comparison To Other Construction Methodsmentioning
confidence: 98%
“…Previously-proposed construction methods for blast shields include regolith berms (Mueller et al, 2009;Morris, 2012;Moses and Mueller, 2021), cast regolith (Benaroya et al, 2012) and microwave heating (Lim et al, 2021). The landing pad for Artemis-class missions is expected to have a diameter of 200 m (with possible reduction to 100 m) (Gelino et al, 2023).…”
Section: Blast Shield Constructionmentioning
confidence: 99%
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“…Previously-proposed construction methods for blast shields include regolith berms (Mueller et al, 2009;Morris, 2012;Moses and Mueller, 2021), cast regolith (Benaroya et al, 2012) and microwave heating (Lim et al, 2021). The landing pad for Artemis-class missions is expected to have a diameter of 200 m (with possible reduction to 100 m) (Gelino et al, 2023).…”
Section: Blast Shield Constructionmentioning
confidence: 99%
“…Such infrastructure projects require significant building materials-yet the transport of mass from Earth to the Moon is extremely expensive, with current prices of around 1.2 mln USD per kilogram (Astrobotic, 2018). Literature suggests in-situ resource utilization (ISRU) for the construction of infrastructure, which can reduce the need of mass transport from Earth, while in return more energy is required (Moses and Mueller, 2021). Methods and materials based on in-situ resources proposed for construction purposes include, for example, microwave heating (Lim et al, 2021), cast regolith (Benaroya et al, 2012), waterless/sulfur concrete (Susante, 2012;Susante and Metzger, 2016;Khoshnevis et al, 2017), 3D-printing (Cesaretti et al, 2014;Yashar et al, 2021) and dry packing of processed rocks (Thangavelu and Adhikari, 2017).…”
Section: Introductionmentioning
confidence: 99%