Proximity to both Scandinavia and mainland Europe makes exporting and importing power rather easy for the Danish system operator, Energinet.dk. This provides Denmark with the flexibility needed to achieve significant penetration of intermittent energy sources like wind while maintaining grid stability.
While the results to-date have been promising, getting to 100 percent renewable energy will still require a significant leap and the official policies that Denmark will use to guide this transition have yet to be delivered. However, there has been some indication at what the ultimate policies may look like. In their report Energy Scenarios for 2020, 2035 and 2050, the Danish Energy Agency outlined four different scenarios for becoming fossil-free by 2050 while meeting the 100 percent renewable electricity target of 2035. The scenarios, which are primarily built around deployment of wind energy or biomass, are:
Wind Scenario – wind as the primary energy source, along with solar PV, and combined heat and power. Massive electrification of the heat and transportation sectors.
Biomass Scenario – less wind deployment that in the wind scenario, with combined heat and power providing electricity and district heating. Transportation based on biofuels.
Bio+ Scenario – existing coal and gas generation replaced with bioenergy, 50% of electricity from wind. Heat from biomass and electricity (heat pumps).
Hydrogen Scenario – electricity from wind used to produce hydrogen through electrolysis. Hydrogen used as renewable energy storage medium, as well as transportation fuel. Hydrogen scenario would require massive electrification of heat and transport sectors, while requiring wind deployment at faster rate than the wind scenario.
Agora Energiewende and DTU Management Engineering, have postulated that this scenario report does in fact show that transitioning the Danish energy sector to 100 percent renewables by 2050 is technically feasible under multiple pathways. However, Danish policy makers must decide before 2020 whether the energy system will evolve into a fuel-based biomass system, or electricity-based wind energy system (they must decided which of the four scenarios to pursue).
Energy Storage Facilities – Denmark
Regardless of which energy policy scenario Denmark decides to pursue, energy storage will be a central aspect of a successful energy transition. There are currently three EES facilities operating in Denmark, all of which are electro-chemical (batteries). A fourth EES facility – the HyBalance project – is currently under construction and will convert electricity produced by wind turbines to hydrogen through PEM electrolysis (proton exchange membrane).
The HyBalance project is the pilot plant undertaking of Power2Hydrogen, a working group comprised of major industry players and academic research institutions aimed at demonstrating the large-scale potential for hydrogen from wind energy. The plant will produce up to 500 kg/day of hydrogen, used for transportation and grid balancing.
Worth noting is the decommissioned BioCat Power-to-Gas project, a pilot plant project which operated from 2014 to 2016 in Hvidovre, Denmark. The project, a joint collaboration between Electrochaea and several industry partners (funded by Energienet.dk), was a 1 MWe Power-to-Gas (methane) facility built to demonstrate the commercial capabilities of methane power-to-gas. The BioCat project was part of Electrochaea’s goal of reaching commercialization in late 2016, however, as of early 2017 no further updates have been given.
Energy Storage Market Outlook − Denmark
The energy storage market in Denmark will be most primed for growth should policy follow the Hydrogen Scenario, where massive amounts of hydrogen production will be needed to eliminate the use of fossil fuels across all sectors.
Renewable energy produced gases (hydrogen, methane) have the potential to balance the electricity grid in two primary ways: balancing supply and demand (“smart grid”), and balancing through physical storage. The smart grid, an intelligent electricity grid where production and consumption are administered centrally, presents significant opportunity for electrolysis technologies as short-term “buffer” storage (seconds to minutes). Bulk physical storage of renewable energy produced gases can act as a longer-term storage solution (hours, days, weeks, months) to help maintain flexibility in a fossil-free energy grid (The Danish Partnership for Hydrogen and Fuel Cells).
Without the hydrogen scenario, the potential for hydrogen-based energy storage in Denmark will be limited. In their 2016 report “potential of hydrogen in energy systems”, the Power2Hydrogen working group concluded that:
hydrogen electrolysers would not provide any significant upgrade on flexibility for renewables integration over today’s sufficiently flexible system, and;
by 2035, with the increased wind production, it was concluded that hydrogen electrolysers would in fact improve system flexibility, allowing for even more extensive penetration of wind energy in the system.
The potential for renewable energy produced gases in Demark is extremely high. There is a very distinct possibility that power-to-gas type of systems will be the linchpin of Denmark’s energy transition. While there appears to be little opportunity in the short-term, there will be extensive opportunity in the medium-to-long-term should the official energy transition policy focus on the hydrogen scenario, or a similar renewable gas based policy.
How do we shape human exploration on Mars to minimize what we must bring with us and to maximize the value and utility of what we bring, and augment it with what is already there?
To provide sufficient fuel for a safe return of the Mars crew, we can produce methane and oxygen on Mars which could be aided by microbes that are brought to Mars. We suggest lightweight perovskite solar panels that may be transported to Mars. In the optimistic scenario, about 18 months are required for the installation of surface solar power and fuel production for the failsafe return after which the crewed mission commences. The pessimistic scenario takes 4 years. To save oxygen, we also suggest Martian perchlorates as rocket fuel component. For later missions’ food supply, we suggest to use lichens as primary colonizers to produce organic rich soil.
Procedure to produce energy on Mars
We suggest the use of in situ Martian resources for the production of methane as ascent and return propellant. Since oxygen generated during electrolysis is not sufficient for a safe return, we also suggest to use algae for the production of oxygen. Algal biomass will be used as soil for food production. Methane producing microbes will be contained in methanogenic electrolysis reactors (MER) while algae will grow in covered craters. The production of methane on Mars is to be carried out autonomously by robots and reactors that will land near the ice-rich polar regions to melt water as electrolyte for low temperature electrolysis. The Mars lander will autonomously construct facilities with the purpose of propellant production to fuel the Mars transfer vehicle which enables transport between Mars surface and Earth orbit. Only when enough propellant for a safe return to Earth has been produced, shall a manned Mars mission begin. Furthermore, methane will be used as energy storage should there be failure of energy collectors such as solar panels. Goal is to erect a 3.5 MW solar power plant on Mars by the end of the first manned mission.
To sustain the life of 6 crew members a power production capacity of 170 kW (see “Surface habitat energy needs”) is required and has highest priority along with fuel production for a safe journey home. The procedure is sketched out in the figure above. It is a stepwise process during which most steps are interdependent and therefore self-accelerating as power production increases. To minimize risk of failure, we recommend at least four independent landers in the circum-polar region of Mars. The polar regions bear the highest surface water content which is crucial for manned explorer missions, methanogenic electrolysis as well as the production of oxygen and biomass. The landers will carry a small nuclear fission device that will begin mining for iron and titanium ores to produce the steel required as structural support for solar panels. First, the lander begins mining for iron ores so that steel production can begin. Graphite or other reduced forms of carbon for steel production will be shipped from Earth because organic matter production on Mars by algae is a slow process. Alternatively, lightweight modular carbon fiber elements to mount solar panels will be brought from Earth to Mars. Once the 170 kW solar plant is established, melting ice for the methanogenic electrolysis reactors (MER) begins. Combined power from the nuclear fission reactor (NFR) and the solar plant will be used. Only when the amount of methane for a failsafe return (Orion capsule size) has been produced, power will be diverted into three equal parts: continue to melt ice for algae, start or continue to mine ores for thermal collectors, continue to produce methane. After enough thermal collectors are produced to pace ice melting with algal growth, electrical ice melting will be shut off. Now, electrical energy is used for steel production to install more solar panels and methane production until sufficient for a comfortable (more payload) return. By this time, the crew is arriving and decides what the highest priorities are. We recommend to focus on accelerating algal growth for oxygen and biomass production as complete independence from Earth requires the production of organic carbon from CO2.
Energy need for the Mars Transfer Vehicle
Fuel produced on Mars will serve 3 purposes:
Failsafe: return of one Orion-sized vehicle
Desired: production of return fuel allowing for less stress (more comfort) during transit
Energy storage at night or power failure
Two options for Mars-Earth return seem possible. (1) Option one was suggested by NASA’s DRA 5.0 and involves one Orion-like vehicle of about 12 tons and a travel speed of 14 km/s. This option requires only one vehicle but provides less comfort for the long journey home and hence, it exposes the crew to higher stress. However, it uses less fuel therefore enables a faster completion of the first Mars mission. (2) We envision a second option that involves two vehicles, one Orion-like lift-off vehicle for transport of 6 crew members into a Mars orbit of 250 km and one transit vehicle to return to Earth. As option two is the preferred option, we recommend to use option one, the Orion-only scenario, as failsafe scenario.
We assume the capacity of a manned Orion capsule with Dragon thrusters (Draco) as reference. The Orion-sized vehicle can carry 6 crew members and has a weight of 12 tons including fuel. For a Mars lift-off, a thrust-mass ratio of at least 5 N/kg will be needed resulting in 60 kN thrust or 150 Draco thrusters to lift 6 crew members. The travel time from Martian surface to a 250 km orbit would be 7 minutes at full thrust. About 600 m3 methane (at Earth atmospheric pressure) would be required for the lift-off. To produce this amount of methane at 210 kW (40 kW nuclear fission and 170 kW solar power, see “Surface habitat energy needs”), 3 years of dedicated fuel production are necessary. The proposed solar power installations of 1,400 m2 perovskite solar cells can produce effectively 170 kW during a Mars day of 8h (that is, 20 kW/m2 can be captured by perovskite panels). Using the same Orion capsule also for the Mars-Earth transit, another 7 minutes or 17,000 km are required to reach the travel speed of 14 km/s and approximately the same for full stop. To produce enough fuel for the Mars-Earth transit, only 3 more days are required. Once enough fuel for the failsafe scenario has been produced, the crew will leave the lower Earth orbit heading for Mars.
For the comfort scenario, we assume the proposed 63-ton crewed payload option from the Mars DRA 5.0 used for Earth-Mars transit. This seems reasonable as most equipment will be left behind on Mars and only the transit habitat, the Orion capsule (for emergencies), engines and fuel are needed. This scenario, however, requires considerably more fuel for which the 210 kW surface power generators must produce methane for at least 42 years. Since this is out of scope, we recommend an extension of the surface power production to 3,500 kW which would reduce the required production of methane to 30 months at 14 km/s travel speed or 12 months at 9 km/s. The reduced stress on the crew justifies the lower travel speed and the higher investment. However, 6.3 tons (corresponding to 0.18 km2) of perovskite solar panels will be required to produce sufficient fuel. About 280 tons of steel are necessary as structural support for this scenario. Since 900 kWh/ton of steel will be consumed for electric smelting, only about one year of steel production using a 40 kW NFR (or 2 months using the full combined 210 kW) justify the increased comfort. The shipment of carbon fiber elements form Earth may completely eliminate the need for steel production in this stage of the mission. The process will be self-accelerating as power production increases during the solar panel assembly process.
To produce methane sufficient for one lift-off, a 200,000 liter MER is required using steel mesh/brush electrodes (anode and cathode) of 2,200 m2 projected surface (see figure below). A modular redundancy system of smaller dimension will improve safety but requires more material. MERs have the theoretical capacity to produce sufficient ascent fuel for one Orion capsule within less than one or two days, if power supply were sufficient. At maximum performance, this reactor would consume about 100 GWh or 220 kWh/mol methane. Microbes will facilitate electrolysis at low temperatures and these microbes will be carried by the Mars lander in small (100 mL) redundant batches. Since the limit for methane production is not the reactor capacity but the electrical power available, doubling the amount of solar panels will half the time required for methane production and so on. To store the so produced methane we recommend to first pressurize water to 200 bar before it is injected into the MER. To extract as from the electrolyte, a small pressure reduction is needed and the so obtained gas phase is then conducted into pressurized steel tanks for later use.
An experimental MER needs to be constructed on Earth to prove this concept. Like the Mars reactor, this experimental MER will be a 5 x 5 m cylindrical reactor of either one or two chambers each. The advantage of the two-chamber system is the separation of oxygen and methane but it requires more water while the single chamber reactor is easier to build and holds less water but O2/CH4 separation is required after production. Unfortunately, the ratio of oxygen to methane is difficult to predict as it depends on the anodic pH. A mass ration greater than 2:1 is required. We therefore propose the use of algae as additional oxygen source (see “Photosynthesis crater to produce oxygen and biomass”). As electrodes brush or spiral steel mesh electrodes will be used. Steel mesh (40 x 40 mesh) produced on Mars will be used having a 1,100 m2 projected surface of each electrode.
Alternative oxidants in cold methane fuel cells or rocket fuel
It is anticipated that oxygen scarcity imposes severe limitations on any manned Mars mission. Oxygen is crucial as propellant and for any human presence. The use of methane for energy storage makes only sense if there is an adequate electron acceptor. While methane can be burnt in turbines at acceptable efficiencies for electricity production, it may also be used in fuel cells. However, no catalysts exist that oxidize methane on electrodes at room temperature or below. The only possible exception are anaerobic methane oxidizing consortia that naturally use biological electron transport chains. The use of biological electron transport chains opens the possibility to capture the energy stored in electrons during transport. Since this is electron acceptor independent, oxidized metal minerals, which are abundant on Mars, can be used as electron acceptors. The disadvantage of this methane fuel cells is that less energy will be captured compared with oxygen. Also, they only exist in theory.
The high acidity on Mars, however, is in favor of reaction, forming additional water from iron oxides and protons using the reductive power of methane. Soluble Fe2+ may be used for electric steel production as the reduction of Fe2+ to Fe0 requires a considerably lower redox potential and therefor lower energy.
Martian perchlorate salts may serve as oxidant in rocket fuel. Ammonium perchlorate and, on Mars, the more prevalent calcium perchlorate are explosive oxidizers. To transform calcium perchlorate into the ammonium salt, ammonium can be produced by a variety of microbial process such as nitrogen fixation (by way of the nitrogenase enzymes) and catabolic ammonification of amino acids or waste urea (by the urease enzyme). Should collection and compression of the photosynthetically derived O2 gas prove impractical for in rocket fuel, our solid oxidizer approach is also submitted. This dual oxidizer strategy will provide for far greater flexibility and more breathable oxygen. Mined perchlorate may also be used to disinfect water.
Photosynthesis crater to produce oxygen and biomass
Oxygenic biophotolysis of water using psychrophilic (cold-loving), dinitrogen fixing cyanobacteria, i.e. blue green algae, grown in covered craters is one proposed plausible means of generating the need for oxygen and biomass. The surplus of oxygen will be required as propellant and component of artificial air in the SHAB. While initially not crucial for a Mars mission, the production of organic matter is useful for more extended missions with larger teams and longer presence. Organic matter is essential for rich soil which, in turn, is pivotal for vegetable food production on Mars. Moreover, cyanobacteria and algae require little engineering and energy which makes them ideal for autonomous production of utility compounds such as organic matter and oxygen.
The amount of damaging cosmic rays and UV can be higher due to the lack of an ozone layer and protective magnetosphere. The amount of cosmic radiation (est. 0.076 Grays per year) is certainly within the tolerable range for many Earthly microbes as it is only around what the interior of the international space station is exposed to. UV light, with its shorter wavelength, can be readily blocked by a thin covering of Martian soil whereas longer wavelengths of photosynthetically active radiation can penetrate further. The microbes will be selectively enriched in their survival zones. Alternatively, a UV protective cover could be used over the crater. The lightweight but durable and robust crater coverings could take the form of an inflatable inverted dome anchored around the crater edge by cables and spikes. The clear upper canopy would admit sunlight but have coating to block harmful radiation while the curved lower surface could be reflective (to maximize photosynthesis) or black to absorb heat. Solar powered gas pumps could adjustably increase the internal gas pressure to accelerate carbon and nitrogen fixation rates and water accumulation from the trace water vapor available.
During the initial surface resource utilization phase (see figure above), the growth of algae is the most time consuming step and therefore the production of liquid water has highest priority. The use of craters will eliminate the need for containers for growing and there reduce the amount of material brought to Mars. Ideally, such craters are equatorial flat water ponds that ensure maximum sunlight capture and minimum water reheating. These preconditions do not align with the initial mission setup (landing near polar ice caps) but should be prepared during the first mission. That is, water pipes from the circum polar regions to the equatorial areas must be constructed. The pipes may need to be heated which requires additional energy or heating the melted water to high temperatures and pressures to prevent ice formation during transport.
Production of water as medium for methanogenic electrolysis and algae
The lack of liquid water is a major hindrance since active metabolism requires a fluid aqueous medium. In addition to the production of methane fuel, melting ice is the greatest challenge for the first manned Mars mission. Liquid water is essential for MERs and algae craters. Hence, all excess of heat or electrical power produced should be directed to melting of ice after methane fuel production is secured. The obtained CO2-rich brine is the electrolyte for MERs. The high acidity is not inhibitory for microbial growth as acidophilicmethanogens and algae were reported from terrestrial environments. Fortunately, the low pH will reduce the electrical overpotential needed for hydrogen generation, which is the intermediate step during methanogenic electrolysis. The low pH, on the other hand, inhibits oxygen formation which is why corrosion of steel anodes is anticipated to become a possible problem. Anode corrosion must be monitored and shall not exceed a certain, yet to be determined, threshold before spent anodes are recycled in steel foundries brought with the first mission.
The low temperatures on Mars that reach only 20°C in equatorial regions also impose a major hurdle on liquid water maintainance. That is, water may need to be heated by parabolic heat collectors to remain liquid. However, Fischer et al. recently found that “when the salts are in contact with water ice, liquid brine forms in minutes, indicating that aqueous solutions could form temporarily where salts and ice coexist on the Martian surface and in the shallow subsurface.” If our crater canopy is fitted with an internally reflective coating in the infrared spectrum small green houses can be created an the brine will remain liquid longer.
The MERs use methanogenic microorganisms for methane production which will be brought to Mars along with algae seeds by the landers. The methanogenic microbes are highly efficient in methane production, resulting in electricity capturing efficiencies close to 100%. Precious metal catalysts are not required. In contrast, for effective oxygen production, platinum or palladium coating may be required on the anodic side of the MERs. Anodic algae appear to be an alternative but need to be further explored. Since the amount of platinum used is very low, it may be transported as salt to Mars and electroplated on steel electrodes once they are ready. Electroplating is an easy procedure so that a robot can accomplish this task within few minutes. However, platinum recycling requires 1-2 days of work of one crew member.
About 280 tons of steel for structural support of solar panels are required (see “Production of steel for structural support of Mars surface components”). The carbon content of steel should not exceed 2.1% to guarantee high stability and therefore we chose 1.5% carbon for Mars steel. That is, about 4 metric tons of carbon are required for steel production. This is the bottleneck of steel production. Assuming cold conditions on Mars comparable to the Antarctic, a good approximation for biomass concentration in brine is 5 mg/m3. At this concentration, nearly 1 billion m3 water need to be processed. While the existing amount of 821,000 km3 would be more than sufficient, it is impossible to melt this amount of ice within the mission’s timeframe using an NFR of 40 kW even if other power sources were counted in. Therefore, parabolic heat collectors could be shipped from Earth as well. At an energetic efficiency of parabolic heat collectors of 80%, 300 tons would be required to melt this amount water within 2 years. Using 10 tons of parabolic collectors, one can melt only 26,000 m3 for algae during 2 years. This is enough to produce 130 g algal carbon in little more than 2 years assuming a constant concentration of 5 mg/m3. It is more efficient to bring 4 tons of graphite to Mars for initial steel production or consider reflecting surfaces other than polished steel.
Alternative use of covered craters to accumulate water using native perchlorates
In light of the considerable difficulties associated with installing long water pipelines to fill craters with water, we outline an elegant alternative strategy for gradually capturing water from the atmosphere using native perchlorates in the Martian sediments.
Halophilic algae tolerate high salt concentrations and low temperatures. Due to the high concentration of CO2 in the native atmosphere the crater covering will amplify the warming effects of this greenhouse gas to prolong the duration of liquid state water needed for nitrogen and carbon fixation. By transporting more soil-derived perchlorates, possibly with crushed water ice deposits, into the covered crater, water can slowly be accumulated. Biologically formed nitrous oxide gas might further accentuate the internal greenhouse warming and thus biological rates of activity.
Perchlorates salts from inside the crater can be recovered from the liquid brine to gradually reduce the salinity of the water. This could be done using parabolic evaporation troughs periodically lifted above the briny surface. Since perchlorates are considered a human toxin, they can be removed by some microbes such as perchlorate reducing bacteria (PRBs) which use percholorates as alternative electron acceptors. Such PRBs could be introduced at a later stage to eventually render the water-filled covered craters non toxic to higher forms of life.
Soil conditioning through phototrophic primary productivity
Lichen and blue green algae have both been used as foods on Earth for hundreds of years. Spirulina is one example of a widely consumed cyanobacterium that uses sunlight to synthesize essential vitamins, antioxidants like beta-carotene and fatty acids from CO2. One major advantage of using a nitrogen fixing cyanobacterium is that they can use solar energy to convert atmospheric nitrogen gas directly into the essential amino acids that future manned missions will need to build and maintain muscle on the Red planet. This will reduce the amount of fuel spent on shuttling food supplies in. Surprisingly, some species of cyanobacteria contain 60% protein per dry gram which is more protein than beefsteak, without the high amount of deleterious cholesterol. Gaseous nitrogen makes up roughly 2.7% of Mars’ thin atmosphere and is available globally. Nitrogen gas is not the only bioavailable form of nitrogen needed to grow oxygenic phototrophs. Nitrates are an ideal fertilizer. The Curiosity rover identified bioavailable nitrates as a significant component of the sediment on Mars. Trace elements are also present in rocks and soil but may require processing.
Production of steel for structural support of Mars surface components
Steel cannot be brought to Mars as there will be at least 2.2 tons of steel necessary for structural support for 1,400 m2 perovskite solar panels. While lightweight carbon fiber modules could be used as structural support, it is possible to produce steel in situ. Steel production on Mars seems an apparent alternative to transport of construction material given the abundance of iron, nickel and titanium on Mars. However, it also requires organic carbon which is to be produced by CO2-fixing algae that grow first in enrichment tanks (transparent plastic bags) and later in covered craters. After dehydrating the algae medium, recycling and reheating it, dry algae pellets will be used as supplement for steel production. The dehydration and reheating process require additional energy which can be provided as heat using parabolic collectors. Parabolic collectors are more efficient in terms of energy capturing and easier to construct as polished steel can be used as opposed to organic Pb/I composites in perovskite solar cells. Steel is then shaped and polished to build parabolic thermal collectors to melt more ice and provide more energy until the NFR and solar panels can be fully replaced by parabolic collectors that can also produce electricity. The production of steel is limited by the amount of organic carbon available. Therefore, we recommend to explore the possibility to use methane gas as reductant and carbon source for steel production. Methane gas production is faster and requires less water resources than algae.
The Mars landers will also mine iron ores and silicates for the production of wires, solar panels and construction materials. Steel will be produced in an induction furnace using iron ores and graphite or organic biomass. Organic biomass from algae tanks will be used for steel production. This organic biomass will also be used for graphite production at a later stage of the mission. Alternative furnace concepts are possible. For example, methane can be used as reductant. Another alternative would be an electric arc furnace or sacrificial graphite electrodes. Graphite can be produced from organic carbon as follows
Organic carbon from CO2 by cold adapted algae
Organic carbon + 800ºC → C
C + SiO2 + 1,400ºC → SiC
SiC + 4,200ºC → graphite
The steel and graphite induction furnaces will be carried by the landers
Energy for initial steel production for the construction of the 170 kW solar plant (see “SHAB energy needs”) is produced by an NFR. A 40 kW reference NFR is recommended. Steel production from iron ore using electric smelting requires 900 kWh per ton of steel. That is, to produce enough structural support for solar panels for 6 people, about 2,000 kWh are necessary or about 3 days of energy production at full performance. This is based on the assumption that steel of 2 mm thickness and 10% of the perovskite area of 1,400 m2 is sufficient. To produce enough structural support for 3.5 MW (0.18 km2) perovskite solar cells needed for the comfortable return option, 280 tons of steel are required. At 50 days of steel production using the entire 210 kW (40 kW NFR + 170 kW solar perovskite life support) are anticipated. To add 1.5% carbon, 4 tons of graphite are necessary which will be carried as cargo from Earth.
Steel is necessary for parabolic heat collectors on site as well. Parabolic heat collectors are required for melting ice for algae growth. The production of steel sufficient for parabolic collectors to melt 1 billion m3 of ice is approximately 600 tons, i.e. 9 additional tons of graphite need to be shipped. To make this amount of steel on Mars another 2 years will be necessary at least. This appears to be the best trade-off between cargo transport and waiting time for a Mars mission but is still an approximation. The algal side product oxygen, also justifies this approach. Since the launch of a manned mission is not dependent on algae production, it is not counted as wait time, which would add another 4 years prior to launch. This shall only demonstrate the feasibility of in situ steel production on Mars. As alternative, the use of methane produced on Mars as carbon and electron source for steel needs to be explored as this may eliminate the need for graphite transport or carbon fiber construction materials are transported to Mars.
Possible perovskite production and reuse of lead produced by the nuclear fission reactor
Lead remnants from the 235U nuclear fission reactor aboard the landers can be used as they are a side product of the radioactive decay of contaminating 238U. There are no confirmed higher concentrations of iodine on Mars and this element needs to be brought in the form of elemental iodine, KI or NaI with the lander to produce the PbI and methyl ammonium iodide. However, since iodine can be replaced by the element chlorine for perovskite production, the initial amount iodine may not need to be replenished because chlorine is an abundant element on Mars.
Solvents required for perovskite cells can be produced in situ using methane gas and acetic acid (also a possible side product of MERs) as precursors as soon as they become available. To bridge the intermediate gap, solvents and organic reactants brought to Mars by the landers may be used. These materials are:
As synthesis of perovskite cells may still be to difficult on Mars, we recommend the transport of these components. As shown below (Surface habitat [SHAB] energy needs), only 9 kg perovskite solar panels will be required. As photo voltaic systems are constantly improved, one can expect better performance and lighter weights in future.
Surface habitat (SHAB) energy needs
The average energy need per capita in the European Union was 150 GJ/year. Although this estimate is likely too high for a permanent colony on Mars we used this as reference herein. A perovskite solar panel operating at 12% efficiency can produce 14 MJ/day/m2 from Mars aphelion 8 hour solar radiation assuming 170 W/m2. That is, 240 m2 methyl ammonium lead halide perovskite solar panels are required to sustain the presence of one person on Mars. This requires 350 g mesoporous TiO2, 370 g Au per capita. The light weight of about 720 g per capita makes a transport of these components from Earth to Mars feasible (8.5 kg total). Mounting the thin solar power collector on a stable steel surface can be achieved on Mars but only if steel is produced in situ. NASA’s Human Exploration of Mars Design Reference Architecture recommends a mission of 6 explorers. That is, at about 1,400 m2 perovskite solar panels or 170 kW capacity will be required only to sustain life of one manned explorer mission. Before installation of these panels, steel will have to be produced on which they can be mounted. For the envisioned larger energy needs, 3.5 MW are necessary and for this, about 6.3 tons of perovskite may be shipped to Mars.
Over the past decade, numerous studies have shown that global warming is roughly proportional to the concentration of CO2 in our atmosphere. In this way one can estimate our remaining carbon budget. This is the total amount of man-made carbon dioxide that can still be released into the atmosphere before reaching a set global temperature limit. The nations of the world agreed on this limit in the 2015 Paris Agreement. It should not exceed 1.5°C, and in any case be well below 2.0°C. However, diverging estimates have been made for the remaining carbon budget, which has a negative impact on policy-making. Now, an international research group of renown climate experts has published a framework for the calculation of the global CO2 budget in Nature. The researchers suggest that the application of this framework should help to overcome the differences when estimating the carbon budget, which will help to reduce uncertainties in research and policy.
Since the fifth report of the Intergovernmental Panel on Climate Change (IPCC), the concept of a carbon budget has become more important as an instrument for guiding climate policy. Over the past decade, a series of studies has clarified why the increase in the global average temperature is roughly proportional to the total amount of CO2 emissions caused by human activity since the Industrial Revolution. In the framework, the research group cites numerous published documents that provide evidence for the linearity of this correlation. This literature has allowed scientists to define the linear relationship between warming and CO2 emissions as a transient climate response to cumulative CO2 emissions (TCRE). The linearity is an appealing concept because of the complexity of the Earth’s response to our CO2 emissions. Additional processes that affect future warming have been included in recent models, among them, for example, the thawing of the Arctic permafrost. These additional processes increase the uncertainty of current climate models. In addition, global warming is not just caused by CO2 emissions. Other greenhouse gases, such as methane, fluorinated gases or nitrous oxide, as well as aerosols and their precursors affect global temperatures. This further complicates the relationship between future CO2.
In the case of global warming caused by CO2, every tonne contributes to warming, whether that ton is emitted in future, now or in the last century. This means that global CO2 emissions must be reduced to zero, and then remain zero. This also means that the more we emit in the next years, the faster we have to reduce our emissions later. At zero emissions, warming would stabilize, but not disappear. It may also reverse. An overdraft of the carbon budget would have to be compensated by removing the CO2 later. One way of removing CO2 from the atmosphere would be a technology called direct air capture, which we reported earlier. Ultimately, this will probably be the only way left, as carbon neutral renewable energy source sources only make up 5% of our energy mix. Establishing a global carbon budget will further highlights the urgency of our clean energy transition. Unfortunately, there is a large divergence when it comes the amount of the CO2 remaining in our carbon budget. In their framework, the researchers cite numerous studies on carbon budgets to maintain our 1.5°C target. Starting 2018, these range from 0 tonnes of CO2 to 1,000 gigatons. For the 2.0°C target, our carbon budget ranges from around 700 gigatons to nearly 2,000 gigatons of remaining CO2 emissions. The aim of the researchers is to limit this uncertainty by establishing a budget framework. The central element is the equation for calculating the remaining carbon budget:
The budget of the remaining CO2 emissions (Blim) for the specific temperature limit (Tlim) is a function of five terms that represent aspects of the geophysical and human-environment systems: the historical man-made warming (Thist), the non-CO2 contribution to the future temperature increase (TnonCO2), the zero emission commitment (TZEC), the TCRE, and an adaptation for sources from possible unrepresented Earth system feedback (EEsfb).
Key choices or uncertainties
Level of understanding
Choice of temperature metrics that allow global warming, the choice of pre-industrial reference and consistency with global climate targets
Medium to high
Historical man-made warming
Incomplete data and methods for estimating the man-made component; see also Tlim
Choice and uncertainty
Medium to high
Non-CO2 contribution to future global warming
The level of non-CO2 contributions coinciding with global net zero CO2 emissions; depends on policy choices, but also on the uncertainty of their implementation
Choice and uncertainty
Non-CO2 contribution to future global warming
Climate reaction to non-CO2 forcers, such as aerosols and methane
Low to medium
The extent of the decadal zero emission commitment and near-zero annual carbon emissions
Transient climate response to cumulative emissions of CO2
TCRE uncertainty, linearity and cumulative CO2 emissions that affect temperature metrics of the TCRE estimate
Low to medium
Transient climate response to cumulative emissions of CO2
Uncertainty of the TCRE linearity, value and distribution beyond peak heating which is affected by cumulative CO2 emissions reduction
Unrepresented Earth system feedback mechanisms
Impact of permafrost thawing and duration as well as methane release from wetlands on geomodels and feedback
It remains a challenge to adequately characterize the uncertainties surrounding the estimates of our carbon budget. In some cases, the reason of these uncertainties is inaccurate knowledge of the underlying processes or inaccurate measurements. In other cases the terminology is used inconsistently. For better comparability and flexibility, the researchers propose to routinely measure global surface air temperature values. This method gives robust data for models and model runs over selected time periods. More detailed comparisons between published estimates of the carbon budget are currently difficult because the original data used for publication often are missing. The researchers therefore propose to provide these in the future along with publications.
Breaking down the carbon budget into its individual factors makes it possible to identify a number of promising pathways for future research. One area of research that might advance this field is to look more closely at the TCRE. Future research is expected to narrow down the range of TCRE uncertainties. Another promising area of research is the study of the correlation between individual factors and their associated uncertainties, for example, between uncertainties in Thist and TnonCO2. This could be achieved by developing methods that allow a more reliable estimate of historical human-induced warming. It is also clear that less complex climate models are useful to further reduce the uncertainties of climate models, and hence the carbon budget. Currently, each factor of the framework presented by yhr researchers has its own uncertainties, and there is no method to formally combine them.
At Frontis Energy, too, we think that progress in these areas would improve our understanding of the estimates of our carbon budget. A systematic understanding of the carbon budget and is crucial for effectively addressing global warming challenges.
Recently, we reported on plans by Australian entrepreneurs and their government to use ammonia (NH3) to store excess wind energy. We proposed converting ammonia and CO2 from wastewater into methane gas (CH4), because it is more stable and easier to transport. The procedure follows the chemical equation:
8 NH3 + 3 CO2 → 4 N2 + 3 CH4 + 6 H2O
Now we have published a scientific article in the online magazine Frontiers in Energy Research where we show that the process is thermodynamically possible and does indeed occur. Methanogenic microbes in anaerobic digester sludge remove the hydrogen (H2) formed by electrolysis from the reaction equilibrium. As a result, the redox potentials of the oxidative (N2/NH3) and the reductive (CO2/CH4) half-reactions come so close that the process becomes spontaneous. It requires a catalyst in the form of wastewater microbes.
To prove our idea, we first searched for the right microbes that could carry out ammonia oxidation. For our experiments in microbial electrolysis cells we used microorganisms from sediments of the Atlantic Ocean off Namibia as starter cultures. Marine sediments are particularly suitable because they are relatively rich in ammonia, free from oxygen (O2) and contain less organic carbon than other ammonia-rich environments. Excluding oxygen is important because it used by ammonia-oxidizing microbes in a process called nitrification:
2 NH3+ + 3 O2 → 2 NO2− + 2 H+ + 2 H2O
Nitrification would have caused an electrochemical short circuit, as the electrons are transferred from the ammonia directly to the oxygen. This would have bypassed the anode (the positive electron accepting electrode) and stored the energy of the ammonia in the water − where it is useless. This is because, anodic water oxidation consumes much more energy than the oxidation of ammonia. In addition, precious metals are often necessary for water oxidation. Without producing oxygen at the anode, we were able to show that the oxidation of ammonium (the dissolved form of ammonia) is coupled to the production of hydrogen.
It was important that the electrochemical potential at the anode was more negative than the +820 mV required for water oxidation. For this purpose, we used a potentiostat that kept the electrochemical potential constant between +550 mV and +150 mV. At all these potentials, N2 was produced at the anode and H2 at the cathode. Since the only source of electrons in the anode compartment was ammonium, the electrons for hydrogen production could come only from the ammonium oxidation. In addition, ammonium was also the only nitrogen source for the production of N2. As a result, the processes would be coupled.
The reaction produces CO2 and methane at a ratio of 1:1. Unfortunately, the CO2 in the biogas makes it almost worthless. As a result, biogas is often flared off, especially in places where natural gas is cheap. The removal of CO2 would greatly enhance the product and can be achieved using CO2 scrubbers. Even more reduced carbon sources can shift the ratio of CO2 to CH4. Nevertheless, CO2 would remain in biogas. Adding hydrogen to anaerobic digesters solves this problem technically. The process is called biogas upgrading. Hydrogen could be produced by electrolysis:
2 H2O → 2 H2 + O2; ∆G°’ = +237 kJ/mol (H2)
Electrolysis of water, however, is expensive and requires higher energy input. The reason is that the electrolysis of water takes place at a relatively high voltage of 1.23 V. One way to get around this is to replace the water by ammonium:
2 NH4+ → N2 + 2 H+ + 3 H2; ∆G°’ = +40 kJ/mol (H2)
With ammonium, the reaction takes place at only 136 mV, which saves the respective amount of energy. Thus, and with suitable catalysts, ammonium could serve as a reducing agent for hydrogen production. Microorganisms in the wastewater could be such catalysts. Moreover, without oxygen, methanogens become active in the wastewater and consume the produced hydrogen:
The low energy gain is due to the small potential difference of ΔEh = +33 mV of CO2 reduction compared to the ammonium oxidation (see Pourbaix diagram above). The energy captured is barely sufficient for ADP phosphorylation (ΔG°’ = +31 kJ/mol). In addition, the nitrogen bond energy is innately high, which requires strong oxidants such as O2 (nitrification) or nitrite (anammox) to break them.
Instead of strong oxidizing agents, an anode may provide the activation energy for the ammonium oxidation, for example when poised at +500 mV. However, such positive redox potentials do not occur naturally in anaerobic environments. Therefore, we tested whether the ammonium oxidation can be coupled to the hydrogenotrophic methanogenesis by offering a positive electrode potential without O2. Indeed, we demonstrated this in our article and have filed a patent application. With our method one could, for example, profitably remove ammonia from industrial wastewater. It is also suitable for energy storage when e.g. Ammonia synthesized using excess wind energy.