Sabatier/Water Electrolysis Process - Revision history

Michel Lamontagne at 13:42, 11 October 2023

2023-10-11T13:42:59Z

Michel Lamontagne: /* Detailed process and alternatives */

2023-10-11T13:37:07Z

Detailed process and alternatives

Michel Lamontagne: /* Current developments */

2021-12-27T18:53:32Z

Current developments

Michel Lamontagne: /* Detailed process and alternatives */

2021-10-28T21:24:40Z

Detailed process and alternatives

Michel Lamontagne at 19:14, 28 October 2021

2021-10-28T19:14:56Z

Michel Lamontagne at 22:31, 12 May 2021

2021-05-12T22:31:38Z

Michel Lamontagne: /* Current developments */

2021-05-12T17:33:51Z

Current developments

Michel Lamontagne at 17:22, 12 May 2021

2021-05-12T17:22:01Z

Michel Lamontagne at 17:21, 12 May 2021

2021-05-12T17:21:35Z

Michel Lamontagne at 17:18, 12 May 2021

2021-05-12T17:18:26Z

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 The electrolysis unit uses an electrolyte, into which water is added. An electrical current between two electrodes splits the water molecules into hydrogen and oxygen, with the hydrogen migrating to one electrode and the oxygen to the other.
-*A unit mass for the electrolytic cells of 4.25 kg/kh/hr has been proposed for the cells(electrolysis).  This puts the cells at 340 kg for this unit.  With additional structural support, piping and controls, two 5000 kg units would be sufficient for the application.
+*A unit mass for the electrolytic cells of 4.25 kg/kh/hr has been proposed for the cells(electrolysis).  This puts the cells at 340 kg for this unit.  With additional structural support, cooling and drying systems (both oxygen and hydrogen are saturated with water at the outlet of the electrolysis unit) piping and controls, two 5000 kg units should be sufficient for the application.
 Heat rejected from the process can be used to melt and heat the input ice, as well as heat the settlement.  However, a lot of the heat is at very low temperatures and may have to be rejected into the Martian environment.

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 The illustration shows just one of the possible process arrangements.  Compression between the Electrolysis unit and the Sabatier unit might be avoided with other choices of equipment, and the storage tanks might be replaced by metal hydride reservoirs.  If dust storms are particularly bad during a synod, the production rate might be too low to complete the refueling of a transportation vehicle.  Use of nuclear power rather than solar power would allow for continuous production and reduce the mass of equipment required.
 The electrolysis unit uses an electrolyte, into which water is added. An electrical current between two electrodes splits the water molecules into hydrogen and oxygen, with the hydrogen migrating to one electrode and the oxygen to the other.
 Heat rejected from the process can be used to melt and heat the input ice, as well as heat the settlement.  However, a lot of the heat is at very low temperatures and may have to be rejected into the Martian environment.

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 A list of current developments for hydrogen generation by electrolysis can be found here (2018)<ref>BUTTLER, Alexander et SPLIETHOFF, Hartmut. Current status of water electrolysis for energy storage, grid balancing and sector coupling via power-to-gas and power-to-liquids: A review. ''Renewable and Sustainable Energy Reviews'', 2018, vol. 82, p. 2440-2454.</ref>.
 [[File:Electrolysis.png|none|thumb|600x600px]]
 ==See Also==

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 Heat rejected from the process can be used to melt and heat the input ice, as well as heat the settlement.  However, a lot of the heat is at very low temperatures and may have to be rejected into the Martian environment.
-A fuel production system using approximately 700 kW of power continuously should be capable of producing the propellant required for a SpaceX Starship vehicle over 2 years, or a Martian synod.
+A fuel production system using approximately 6-700 kW of power continuously should be capable of producing the propellant required for a SpaceX Starship vehicle over 2 years, or a Martian synod.
 Another alternative is the use of the [https://doi.org/10.1016/j.ijhydene.2017.09.035 Sulfur Iodine cycle] which uses thermal energy to split water into H<sub>2</sub> and O<sub>2</sub>. This generally requires a [http://www.academia.edu/download/48701931/ACT-RPR-PRO-1107-LS-NTER.pdf turboinductor] to create a sufficiently hot gas stream from the much lower output temperature of a standard nuclear reactor such as a [https://www.nasa.gov/directorates/spacetech/kilopower/ KiloPower]. The primary advantage of this method is that it can more directly use the nuclear energy, reducing the requirement for large scale electricity generation.

← Older revision		Revision as of 19:14, 28 October 2021
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	Heat rejected from the process can be used to melt and heat the input ice, as well as heat the settlement. However, a lot of the heat is at very low temperatures and may have to be rejected into the Martian environment.		Heat rejected from the process can be used to melt and heat the input ice, as well as heat the settlement. However, a lot of the heat is at very low temperatures and may have to be rejected into the Martian environment.
		+	A fuel production system using approximately 700 kW of power continuously should be capable of producing the propellant required for a SpaceX Starship vehicle over 2 years, or a Martian synod.

	Another alternative is the use of the [https://doi.org/10.1016/j.ijhydene.2017.09.035 Sulfur Iodine cycle] which uses thermal energy to split water into H<sub>2</sub> and O<sub>2</sub>. This generally requires a [http://www.academia.edu/download/48701931/ACT-RPR-PRO-1107-LS-NTER.pdf turboinductor] to create a sufficiently hot gas stream from the much lower output temperature of a standard nuclear reactor such as a [https://www.nasa.gov/directorates/spacetech/kilopower/ KiloPower]. The primary advantage of this method is that it can more directly use the nuclear energy, reducing the requirement for large scale electricity generation.		Another alternative is the use of the [https://doi.org/10.1016/j.ijhydene.2017.09.035 Sulfur Iodine cycle] which uses thermal energy to split water into H<sub>2</sub> and O<sub>2</sub>. This generally requires a [http://www.academia.edu/download/48701931/ACT-RPR-PRO-1107-LS-NTER.pdf turboinductor] to create a sufficiently hot gas stream from the much lower output temperature of a standard nuclear reactor such as a [https://www.nasa.gov/directorates/spacetech/kilopower/ KiloPower]. The primary advantage of this method is that it can more directly use the nuclear energy, reducing the requirement for large scale electricity generation.

← Older revision		Revision as of 22:31, 12 May 2021
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	[[File:Propellant production.png\|thumb\|600x600px\|Schematic of Methane production system for a Single SpaceX Starship over a period of two years, at about 150 tonnes of methane per year.]]		[[File:Propellant production.png\|thumb\|600x600px\|Schematic of Methane production system for a Single SpaceX Starship over a period of two years, at about 150 tonnes of methane per year.]]
		+	__NOTOC__
	The [[Sabatier reaction]] and [[Electrolysis\|water electrolysis]] are used to convert atmospheric carbon dioxide and water extracted from regolith, or the atmosphere, into propellant. [[Hydrogen]] shipped from [[Earth]] could also be used in certain scenarios to avoid the need for the electrolysis process<ref>Compact and Lightweight Sabatier Reactor for Carbon Dioxide Reduction https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120016419.pdf</ref>.		The [[Sabatier reaction]] and [[Electrolysis\|water electrolysis]] are used to convert atmospheric carbon dioxide and water extracted from regolith, or the atmosphere, into propellant. [[Hydrogen]] shipped from [[Earth]] could also be used in certain scenarios to avoid the need for the electrolysis process<ref>Compact and Lightweight Sabatier Reactor for Carbon Dioxide Reduction https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120016419.pdf</ref>.

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 ==Current developments==
 The Helmeth<ref>http://www.helmeth.eu/index.php</ref> program in Europe is developing a version of the Sabatier/Water electrolysis process for Power to Gas applications.  The EU project HELMETH coordinated by KIT has demonstrated that high-temperature electrolysis and methanation can be combined in a power-to-gas process with an efficiency of more than 75 percent<ref>http://www.helmeth.eu/images/joomlaplates/documents/PI_2018_009_Power%20to%20Gas%20with%20High%20Efficiency.pdf</ref>.
 ==See Also==

@@ Line 8: / Line 8: @@
 The reaction takes place in the presence catalysts at a temperature between 300 and 400C.  A [[nickel]] [[catalyst]] is the most likely candidate, or a catalyst made out of [[ruthenium]] or [[alumina]] might be used.
-The Sabatier process produces a ratio of 4:1 of oxygen to methane, slightly more than the ratio used for propulsion, that is between 3.6 and 3.8 :1.  Excess oxygen can be used for the colony atmosphere or stored for future use.
+The Sabatier process produces a ratio of 4:1 of oxygen to methane, slightly more than the ratio used for propulsion, that is between 3.6 and 3.8 :1.  Excess oxygen can be used for the settlement atmosphere or stored for future use.
 ==Detailed process and alternatives==

← Older revision		Revision as of 17:21, 12 May 2021
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−	[[File:Propellant production.png\|thumb\|600x600px\|Schematic of Methane production system for a Single SpaceX Starship over a period of two years~~. Electrolysis and hydrogen storage are off the shelf. Sabatier reactor needs to be developed~~.]]	+	[[File:Propellant production.png\|thumb\|600x600px\|Schematic of Methane production system for a Single SpaceX Starship over a period of two years, at about 150 tonnes of methane per year.]]
	The [[Sabatier reaction]] and [[Electrolysis\|water electrolysis]] are used to convert atmospheric carbon dioxide and water extracted from regolith, or the atmosphere, into propellant. [[Hydrogen]] shipped from [[Earth]] could also be used in certain scenarios to avoid the need for the electrolysis process<ref>Compact and Lightweight Sabatier Reactor for Carbon Dioxide Reduction https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120016419.pdf</ref>.		The [[Sabatier reaction]] and [[Electrolysis\|water electrolysis]] are used to convert atmospheric carbon dioxide and water extracted from regolith, or the atmosphere, into propellant. [[Hydrogen]] shipped from [[Earth]] could also be used in certain scenarios to avoid the need for the electrolysis process<ref>Compact and Lightweight Sabatier Reactor for Carbon Dioxide Reduction https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20120016419.pdf</ref>.

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 ==Sabatier reactor==
-[[File:Helmeth implementation prototype.jpg|thumb|A view of the Helmeth Sabatier reactor.  CO2 is fed into the tube bundles filled with catalyst and cooled by water phase change to steam.  The steam then feeds a electrolysis unit]]
+[[File:Helmeth implementation prototype.jpg|thumb|A view of the Helmeth Sabatier reactor.  CO2 is fed into the tube bundles filled with catalyst and cooled by water phase change to steam.  The steam then feeds a electrolysis unit|alt=|500x500px]]
-A Sabatier reactor includes a catalyst, generally [[nickel]]. The general form of the reactor is tubular, to increase the contact surfaces.  The process operates at high pressure (TBC) and temperature (300-400C). There is an interesting synergy possible in combining the Sabatier process with electrolysis.  Some of heat heat from the process could be used to preheat the water for the electrolysis.  High temperature electrolysis may be more efficient than electrolysis at lower temperatures.
+A Sabatier reactor includes a catalyst, generally [[nickel]]. The general form of the reactor is tubular, to increase the contact surfaces.  The process operates at high pressure (30 Bar) and temperature (300-400C). There is an interesting synergy possible in combining the Sabatier process with electrolysis.  Some of heat heat from the process could be used to preheat the water for the electrolysis.  High temperature electrolysis should be more efficient than electrolysis at lower temperatures.
-If [[nickel]] is produced in-situ on Mars, additive printing could be used to prepare replacement electrodes for the Sabatier process.
+If [[nickel]] is produced in-situ on Mars, additive printing could be used to prepare catalytic elements for the Sabatier process.  The nickel might serve as well to produce electrodes for the electrolysis process.
-== Current developments ==
+==Current developments==
 The Helmeth<ref>http://www.helmeth.eu/index.php</ref> program in Europe is developing a version of the Sabatier/Water electrolysis process for Power to Gas applications.  The EU project HELMETH coordinated by KIT has demonstrated that high-temperature electrolysis and methanation can be combined in a power-to-gas process with an efficiency of more than 75 percent<ref>http://www.helmeth.eu/images/joomlaplates/documents/PI_2018_009_Power%20to%20Gas%20with%20High%20Efficiency.pdf</ref>.