Atmospheric processing describes the extraction of substances out of the Martian atmosphere and the usage as raw material for further processing. Unlike surface and sub-surface mining, the atmospheric mining does not require the movement of large amounts of regolith or rock with heavy machinery, nor is expensive transport per rover or railroad necessary. The atmosphere can simply be sucked in through a pipe at every location, and the processing is done inside of buildings. Also, the maintenance of all the mining machinery is in-house, which is a major safety advantage.
Collection of Atmosphere
There are a number of ways the martian atmosphere can be processed to separate it into its individual components for process use. Mechanical compression is one of the main possibilities for large scale operations
In mechanical compression systems, a fan collects martian atmosphere and passes it through filters to separate out the dust. Then a compressor increases the pressure of the atmosphere to reach a point when water can be condensed out. Then a second compressor increases the pressure to the liquefaction point of CO2. The liquid CO2 is removed, and the leftover gases can be cooled further, to condense out into their liquid phases.
Compression from the initial atmospheric pressure of 600 Pa to 0,1 bar (10 kPa, or 1/10 Earth atmosphere) heats the atmosphere to 100°C but also creates adequate conditions for the condensation of water when it is cooled to about 40°C. It can then collect at the bottom of a pressure vessel and be removed. A second compressor increases the gas pressure to a bit above 5,1 bar (520 kPa) but also boosts the temperature to over 800°C. 530 kPa is the lowest pressure at which CO2 can change from a gas to a liquid (at lower pressures it turns directly into a solid), at about -57°C. The liquid carbon dioxide can then be separated by gravity from the other gasses. The total compression ratio from 600 to 520 000 Pa is about 860 times.
An exit temperature for a compressor of 800°C is extremely high. Intermediate cooling with isobaric compression (change of volume with constant pressure) may be required to reduce the exit temperatures of the compressors.
The change from a gas phase to a liquid phase is condensation. The compressors create a pressure environment where cooling the gas condensates one of the fractions of the atmosphere. The first gas to condensate out is water, at 40°C for 10 kPa pressure. After an increase in pressure, the hot dry gas is cooled further to condense the CO2 , at -57°C for 520 kPa. The condensed liquid CO2 can be removed by gravity. Nitrogen at 510 kPa will liquefy at -170°C, and Argon at about the same temperature, so care must be taken if we want to keep these two gases separate. The next gas to condense out is Oxygen. All of the cooled gas may be used for process purposes, or some of the gases may be released back into the atmosphere. The expansion of the gas back to atmospheric pressure produces a cooling effect that can be used in the process to condensate out the atmospheric gases.
Desiccation might be used as an alternative to compression for water removal. A desiccant bed, or a desiccant coated wheel, can be inserted into the air-stream, after filtration. The desiccant captures the water, that is later removed from the desiccant using heat in a regenerative process. This might use the heat from the secondary compression, that is significant at 520 kPa, rather than mechanical work.
The Martian atmosphere contains variable amounts of dust, which consists of minerals lifted by wind from the surface regolith. Electrostatic filters, cyclonic separators or dust collectors with fabric filters will be used to remove the dust to prevent it from damaging the equipment.
The 0.03 % water vapor (H2O) is equivalent to about 10 % air humidity after adiabatic compression and cooling to around 1°C. A device similar to an air dehumidifier can be used to extract this water.
The balance of the remaining gas after carbon dioxide condensation contains mostly nitrogen and argon. This mixture can serve as a buffer for oxygen to produce a breathable atmosphere. remaining traces of Carbon monoxide must be catalytically removed if the gas is to be used for the settlement atmosphere.
Argon is useful for industrial processes that must be performed in an inert atmosphere. It can also be used for electric rocket propulsion. It may be used as a complement for nitrogen in a martian settlement if it proves to be safe for that purpose.
Oxygen in used for the creation of the settlement atmosphere or for a large number of industrial processes. The settlement operations may be oxygen rich, so excess oxygen may be returned to the martian atmosphere.