48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2010
DOI: 10.2514/6.2010-799
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In Situ Resource Utilization on Mars - Update from DRA 5.0 Study

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Cited by 16 publications
(11 citation statements)
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“…Trade studies over the past 15 years have identified ‘Mars atmospheric CO 2 [as] important for O 2 and hydrocarbon fuel production, nitrogen (N 2 ) [as] important as a buffer gas for life support, [and] argon (Ar) [as] useful as an inert gas for science experiments and propulsion system purging’ [ 83 ]. Accordingly, carbon-based fuels such as methane, methanol, benzene/toluene and Fischer–Tropsch products have been closely examined for their Mars utility [ 84 ]. Of these, a (liquefied) methane–(liquefied) oxygen combination is the currently selected ascent propellant, based upon its propulsion performance and in situ production process complexity [ 84 , 85 ].…”
Section: Propellant Generation In Spacementioning
confidence: 99%
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“…Trade studies over the past 15 years have identified ‘Mars atmospheric CO 2 [as] important for O 2 and hydrocarbon fuel production, nitrogen (N 2 ) [as] important as a buffer gas for life support, [and] argon (Ar) [as] useful as an inert gas for science experiments and propulsion system purging’ [ 83 ]. Accordingly, carbon-based fuels such as methane, methanol, benzene/toluene and Fischer–Tropsch products have been closely examined for their Mars utility [ 84 ]. Of these, a (liquefied) methane–(liquefied) oxygen combination is the currently selected ascent propellant, based upon its propulsion performance and in situ production process complexity [ 84 , 85 ].…”
Section: Propellant Generation In Spacementioning
confidence: 99%
“…Accordingly, carbon-based fuels such as methane, methanol, benzene/toluene and Fischer–Tropsch products have been closely examined for their Mars utility [ 84 ]. Of these, a (liquefied) methane–(liquefied) oxygen combination is the currently selected ascent propellant, based upon its propulsion performance and in situ production process complexity [ 84 , 85 ]. Methane's density-specific impulse is higher than that of hydrogen, which is an important consideration for compact, low-volume engine feasibility.…”
Section: Propellant Generation In Spacementioning
confidence: 99%
“…Case 3 adds in oxygen and water requirements for life support. The oxygen numbers are based on [9] while the water numbers are based on [10] which defines a so-called 'water rich' Mars scenario where Mars water is used for everything from drinking to laundry. The most conservative case was used which assumes an open-loop ECLSS system.…”
Section: Case Title Descriptionmentioning
confidence: 99%
“…Electrolytic cells offer the very interesting opportunity of obtaining either of them, or even both in the very same process, in this case delivering syngas. Electrolysis of CO 2 , H 2 O, and co-electrolysis of CO 2 /H 2 O mixtures were first demonstrated in the 1960s under NASA contracts for the purpose of O 2 production for life support and propulsion in spacecraft [72]. It is known that all electrolyzers have the ability to split CO 2 as they do H 2 O molecules, although at different rates.…”
Section: Electrochemical Synthesismentioning
confidence: 99%
“…The RWGS and FT Ethylene Reactor concept for ISRU (In-Situ Resource Utilization) space mission is an inspiring approach [72]. Carbon dioxide acquired from the Martian atmosphere is reacted with hydrogen by reverse water gas shift (RWGS):…”
Section: A Space Mission Approachmentioning
confidence: 99%