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Yes, smelting iron ore (regolith) on Mars to make girders for dome supports is a viable concept, with recent research showing scientists can extract pure iron and iron alloys from simulated Martian soil using Mars-like conditions (low pressure, high heat), making in-situ resource utilization (ISRU) possible for building habitats, though domes themselves face tension challenges requiring strong materials like steel.
The Process:
Extracting Iron: Researchers heat Martian regolith simulant (like that from Gale Crater) in a furnace simulating Mars's low atmospheric pressure.
Smelting: At around 1000°C, pure iron forms; at 1400°C, liquid iron-silicon alloys are produced, similar to Earth's processes but optimized for Mars.
Refining: This metal can then be separated from slag and potentially used to create steel or other structural components.
Why It Matters for Domes & Girders:
Reduces Earth Reliance: Instead of shipping massive amounts of steel, future colonists can "live off the land" (ISRU).
Structural Strength: Martian domes, pressurized by internal air, are under tension (trying to tear themselves apart) and need strong materials like steel for reinforcement, making locally produced girders crucial.
Key Takeaway: This technology moves beyond just oxygen production (like NASA's MOXIE) to creating essential building materials, making self-sufficient Martian colonies more feasible
Making iron girders on Mars for dome support involves In-Situ Resource Utilization (ISRU), requiring specialized equipment like furnaces (maybe electric or solar-powered), systems to extract iron from regolith (dirt), a carbon source (from CO2), and technologies for refining and shaping into beams, likely using methods like additive manufacturing (3D printing) or casting, all while managing extreme Martian conditions. Key steps include ore processing, reduction (removing oxygen), alloying for strength, and fabrication into structural components.
Required Processes & Equipment
Regolith Processing & Mining:
Equipment: Rovers with drills, excavators, and material handlers to collect iron-rich regolith (Martian dirt).
Process: Separation of iron-bearing minerals from silica and other materials.
Iron Extraction (Smelting/Reduction):
Carbothermic Reduction: Heating the ore with a carbon source (from Martian CO2) in a furnace to produce molten iron.
Hydrogen Reduction: Using hydrogen (produced on Mars) as a reducing agent.
Molten Regolith Electrolysis: An alternative method.
Equipment: High-temperature furnaces (possibly solar-powered or electric), systems to generate reducing agents (C, H).
Technology: The MMOST (Moon to Mars Oxygen and Steel) system is a NASA-backed concept for this.
Steelmaking & Alloying:
Process: Adding specific elements (like silicon, manganese, chromium) to the iron to create strong steel suitable for construction.
Equipment: Alloying furnaces, refining vessels.
Fabrication (Making Girders):
Additive Manufacturing (3D Printing): Printing complex shapes like girders directly from metal powder or molten metal.
Casting: Pouring molten steel into molds.
Machining: Shaping hardened steel components.
Equipment: Industrial 3D printers, casting molds, robotic arms.
Energy & Infrastructure:
Solar Arrays/Nuclear Power: To provide the immense energy needed for heating and processing.
Habitats & Workshops: Pressurized environments for equipment and personnel.
Key Martian Advantages/Challenges
Abundant Iron: Iron oxides are common in Martian regolith.
Atmosphere: The CO2 atmosphere provides carbon for steelmaking.
Low Oxygen/Water: Less rust/corrosion on finished steel.
Challenges: Low atmospheric pressure, extreme temperatures, and the need to transport initial complex equipment from Earth.
The concept of 3-axis interlocking bricks for building structures like parabolic domes on Mars is an active area of research within extraterrestrial construction, focusing on using local resources (regolith) and robotic assembly.
Key Research & Design Concepts
Interlocking Design: The primary goal of interlocking bricks is to create strong, form-fitting, and compression-dominated structures without relying heavily on traditional Earth-based mortars or adhesives, which are problematic in Mars's thin atmosphere. The wedging action of correctly shaped blocks provides stability.
3-Way Interlocking Units: Architectural and engineering research has explored using "3-way interlocking units" or "universal joints" to map non-planar, complex geometries like hemispherical or parabolic domes. These designs maximize surface contact and prevent horizontal movement, often involving complex computational design (CAD) and robotic fabrication processes (like multi-axis CNC or 3D printing with robotic arms) to achieve the precise, varied angles required for a curved surface.
Material Sourcing (ISRU): To minimize materials shipped from Earth, researchers use Martian regolith simulants to create "space bricks". Methods include:
Compression: Applying high pressure to iron-oxide-rich Martian simulant causes the nanoparticles to bind, forming solid bricks without any additional binders.
Biopolymers: Using synthetic living materials (like cyanobacteria and fungi) to "glue" regolith particles together into building blocks.
3D Printing/Sintering: Using high-powered lasers or a binding agent (such as sulfur cement) to fuse regolith layers, often employing 3-axis or 4-axis Cartesian robots to print specific material paths.
Specific Project Examples
TESSERAE Tiles: Research at MIT has focused on self-assembling tiles called TESSERAE, which use embedded magnets and specifically beveled faces to automatically assemble into complex shapes, such as a "buckyball" or dome structure, in microgravity or a controlled environment.
NASA 3D Printed Habitats: NASA has sponsored competitions and research into large-scale additive manufacturing (3D printing) of entire habitats using Martian regolith materials, often resulting in dome or vault designs (e.g., the Mars Dune Alpha habitat).
The creation of actual physical 3-axis interlocking "pieces" is generally part of specialized academic research and robotic fabrication workflows, not commercially available products in the traditional sense, as the geometry is highly specific to the intended dome's exact curvature and size
3-way Interlocking Units on Hemispherical Dome Surface

Sort of like a tongue and grove but not only the top an bottom but also the ends of the block sized brick.

prefabbed log cabin wall
Dome would be double walled

I was about town today and looked at the brick structures that I have to view the methods employed in construction.
the brace build outs are part of its thick wall construction. which have granite corner footing stone and angled head toppers as well.

The other buildings with in the area are only 3 stories high.
Also the rocket system that supplies must be logical in mass management of items that are required to give the build up of equipment, resources and more for the construction to even begin for a manned sustained presence.

A Mars habitat mission requires robust life support (air, water, power), radiation shielding, extreme thermal control, and durable structures to withstand Mars' harsh environment, plus systems for food, waste, communication, and medical care; crew needs include psychological resilience, STEM skills, and physical fitness, as seen in NASA's simulations focusing on teamwork, resource limits, and isolation challenges to prepare for long-duration stays and self-sufficiency.
Key Habitat & System Requirements
Life Support: Closed-loop systems for air (CO2 scrubbing, oxygen generation) and water recycling, plus reliable power (solar, nuclear) for continuous operation.
Structure: Must handle extreme cold (avg. -62°C), low atmospheric pressure, dust, and significant internal pressure forces (over 2,000 psf).
Resources: In-situ resource utilization (ISRU) for water/fuel, food production (hydroponics), and efficient waste management.
Protection: Shielding against cosmic and solar radiation, dust mitigation systems, and robust thermal control.
Interfaces: Commonality with other vehicles (rovers, landers) for power, data, and crew transfer.
Crew & Operational Requirements (NASA Analog Missions)
Crew Profile: Healthy, motivated US citizens/residents (ages 30-55), non-smokers, with STEM Master's degrees or equivalent experience, and strong teamwork/problem-solving skills.
Psychological Health: Focus on managing isolation, confinement, interdependence, communication delays, and developing strong interpersonal skills.
Operations: Simulate realistic stressors like equipment failures, resource limitations, and communication blackouts for long durations (e.g., ~378 days).
Mission Class & Duration
Opposition Class: Shorter stays (e.g., 30 days at Mars) with Venus flyby.
Conjunction Class: Longer stays (e.g., 500+ days at Mars) due to orbital mechanics, requiring more self-sufficiency
Moon to Mars (M2M) Habitation Considerations
What's the Bare Minimum Number of People for a Mars Habitat?
Minimum Acceptable Net Habitable Volume for Long‐Duration Exploration Missions
Sustaining Human Presence on Mars Using ISRU and a Reusable Lander
Basalt Crushing Plant: Process, Machines, and Price

Final product sizes and applications
0–5 mm: Manufactured sand for concrete, dry-mix mortar, asphalt mix
5–10 mm: High-grade road base, permeable concrete
10–20 mm: Municipal projects, ready-mix concrete plants
20–31.5 mm: Railway ballast, highway base, mass concrete
>31.5 mm: Returned for re-crushing to ensure proper gradation
if the top of the dome inside contains the inlet for the air heat to enter and a fan pushes that heat away towards the cold radiator tubing and once it exits it the air exits at the base of the dome we have the loop that is the way to go. Attachment point are to the building structures for the most part rather than connection to the dome itself.
This is not a ceiling fan but a duct fan that pulls the air from the top of the dome into the vent system to send it to the cooling exchanger.
Ceiling fan AI response.
For a structure with a 200 m (656 ft) diameter and 120 m (394 ft) tall parabolic dome, standard High-Volume, Low-Speed (HVLS) ceiling fans, typically with diameters up to 7.3 meters (24 feet), would be used in a calculated array to provide effective air circulation. Multiple fans, rather than a single massive fan, are required due to the immense size of the space.
Step 1: Calculate the Floor Area and Assess Fan Coverage The floor area of the dome is a circle with a radius of 100 m:\(\text{Area}=\pi \times \text{radius}^{2}=\pi \times 100^{2}\approx 31,416\,\text{m}^{2}\,(338,166\,\text{ft}^{2})\)A single large HVLS fan (e.g., 7.3 m diameter) typically covers between 900 and 1,500 square meters. For cooling purposes, the coverage area is roughly five times the fan's diameter for large-blade fans, but for destratification (air mixing in very high spaces), it can be up to ten times.
Step 2: Determine the Number and Placement of Fans Given the vast area, an array of fans is necessary. The general guideline is to space fans a distance equal to at least one fan diameter apart, or up to three times the diameter depending on the manufacturer and application. For consistent coverage, a grid pattern is ideal. For such a massive, open space, consulting with an HVLS expert for a custom layout drawing is crucial. The number of 7.3-meter (24-foot) fans could range from 21 to over 30 to cover the entire area effectively, depending on specific airflow requirements and building obstructions.
Step 3: Consider Ceiling Height and Fan Mounting The 120 m (394 ft) ceiling is extremely high. While fans perform well when mounted between 6 and 12 meters (20 to 40 feet) above the floor, longer downrods might be needed to position the fans within the occupied zone for optimal air movement. The fans must also maintain safe clearance from the floor (at least 3 m or 10 ft) and other structural elements.
Answer: For a parabolic dome ceiling with a 200 m diameter and 120 m height, multiple HVLS fans with diameters typically ranging from 6.1 meters to 7.3 meters (20 to 24 feet) would be required. The exact number and strategic placement of fans, likely exceeding two dozen units, should be determined through a professional airflow study to ensure uniform air circulation and temperature control
Commercial 7m (7-meter) fans refer to large industrial fans, often HVLS (High-Volume, Low-Speed) ceiling fans, used for cooling vast spaces like warehouses, factories, malls, and arenas, providing massive airflow (measured in CFM) for comfort and energy efficiency in huge commercial areas. You'll find them as massive ceiling units or powerful pedestal/wall-mounted fans designed for serious air movement, not typical home use, with high CFM ratings (thousands) for effective cooling.
Key Characteristics:
Size & Type: Look for HVLS fans (often 7 feet or more in diameter) or large pedestal/wall fans, not standard residential ceiling fans.
Airflow (CFM): Measured in Cubic Feet per Minute; higher CFM means more air moved, crucial for large spaces (e.g., 7000+ CFM is common).
Applications: Warehouses, factories, gyms, shopping centers, agricultural buildings, and large event spaces.
Benefits: Better air circulation, reduced heat, improved comfort, and energy savings over traditional AC in large buildings.
Where to Find Them:
Home Improvement Stores: The Home Depot offers large industrial ceiling fans.
Online Marketplaces: Alibaba.com has many manufacturers for 7m industrial fans.
Specialty Retailers: Amazon.com (for large pedestal/wall fans) and industrial fan suppliers.
When searching, use terms like "HVLS fan," "industrial ceiling fan," "large commercial fan," or specify CFM and diameter (like 7ft or 7m) for best results
Insulation for mars has similarities to basements in the north. The concrete walls are insulated with close cell foam on both sides of the cellar. The depth of the foam is R15 or 4" thick so as to get soil temperature isolated from the frozen ground that happens in deep winter.
Open basalt insulation would need to be inside 2 brick wall assemblies and the distance between them is over 16" to get to R49 or better.
The depth of the regolith berm is close to this but is not isolating but conductive to the surface air temperatures.
The issue is we have not delivered the cargo to do the mining, processing or smelting of the ore to even think about using metal beams as part of dome structure. Solving that as I started to do means you have a plan for what is required.
Boring plus Drilling tech, 3D printing insitu and Tunneling equipment
Need radar sub surface viewing for what is beneath the surface. To detect large rocks and depth to bedrock or underground voids.
3D printing of dome-shaped habitats on Mars using basalt-based materials is a leading area of research for in-situ construction. This approach leverages the abundant basaltic rock and regolith found on the Martian surface to create a structurally sound, radiation-shielding building material, eliminating the need to transport heavy materials from Earth.
Construction Techniques
The primary method involves additive manufacturing (3D printing) using robotic systems deployed autonomously before human arrival.
Material Acquisition and Processing: Robots collect basalt rocks and regolith (crushed rock and dust) and process them into a usable feedstock. One method involves melting the basalt in a furnace and pulling it into fibers, which are then combined with a binder.
Binding Agents: To create a cohesive, printable "ink," the basalt material is often mixed with a binder. In various NASA challenges, teams have experimented with:
Polymer composites: Combining basalt fibers with polylactic acid (PLA) or other recyclable plastics, which can potentially be synthesized from plants grown on Mars.
Geopolymers/Cements: Using fast-setting metakaolin geopolymer cement formulations.
Printing Process: The material is extruded layer by layer by a gantry-style or robotic arm printer, building the habitat from the ground up. The dome shape itself is a functional design choice, as the curved walls help to withstand the significant pressure difference between the internal human-habitable atmosphere and the near-vacuum Martian environment.
Advantages of Basalt for Mars Habitats
Radiation Shielding: Cooled basalt has a high density, which provides superior protection from electromagnetic space radiation and micrometeorites compared to more porous materials.
Structural Integrity: Basalt fiber-reinforced composites can be several times stronger than traditional concrete, providing robust structural elements.
Thermal Regulation: The material has a low coefficient of thermal expansion, advantageous for the extreme temperature swings on Mars.
Airtight Seal: Basalt's low permeability makes it suitable for forming the necessary hermetic seal to maintain a pressurized, life-supporting internal atmosphere.
Current Status and Research
Research has largely been driven by competitions like the NASA 3D-Printed Habitat Challenge. While material processing and 3D printing techniques have been successfully demonstrated using Martian regolith simulants on Earth, the practical challenge of establishing the energy-intensive processing equipment (like high-temperature furnaces) on Mars remains a significant engineering hurdle.
Additive Construction using Basalt Regolith Fines
Mars X-House: Design Principles for an Autonomously 3D
THREE DIMENSIONAL (3D) PRINTED HABITAT, PHASE 3
Basalt is a very hard, abrasive rock, so its processing for 3D printing requires robust, industrial-grade crushing and grinding machinery to produce the necessary fine powder or granule sizes. Typical crushing sequences involve multiple stages of specialized equipment, rather than a single machine.
Equipment for Basalt Crushing
A multi-stage process is typically used to break down large basalt rock into fine powder or granules suitable for applications such as fiber production or as an aggregate in 3D printed concrete.
Primary Crushing: Jaw Crushers
Purpose: The first stage of size reduction for large, raw basalt pieces.
Description: Jaw crushers are built strong with a deep crushing chamber to handle large, tough lumps of rock effectively, reducing them to sizes manageable by the next stage (e.g., from a meter down to a few inches).
Secondary/Tertiary Crushing: Cone Crushers or Impact Crushers
Purpose: To further reduce the basalt to a more uniform, smaller aggregate size (e.g., down to 0-40mm).
Description:
Cone crushers are highly recommended for hard, abrasive materials like basalt due to their durability and efficiency in producing a uniform, cubic product with lower wear rates than impact crushers.
Impact crushers can also be used, especially for shaping the material into a cubical form, but they tend to experience higher wear when processing hard basalt.
Fine Grinding (Milling): Ball Mills or Vertical Roller Mills
Purpose: To achieve the fine, micron-level powder needed for specialized 3D printing material composites, fillers, or fiber production.
Description: These machines use balls or high pressure to pulverize the basalt into the extremely fine particles required for additive manufacturing processes.
Screening and Classifying Equipment
Purpose: To sort the crushed material by size and ensure the final product meets the required specifications for 3D printing projects.
Description: Vibrating screens are used after each crushing stage to separate the desired product sizes from oversized material, which is then recirculated for further crushing. Air classifiers or washers may also be used to remove impurities and achieve specific material properties.
Considerations for 3D Printing Projects
Particle Size and Shape: 3D printing requires a consistent and specific particle size distribution (PSD). The equipment used must be able to produce material within narrow tolerances.
Material Abrasiveness: Basalt is highly abrasive, with a Mohs hardness of 5-9. Equipment must have heavy-duty construction and wear-resistant liners (e.g., tungsten carbide components) to withstand the wear and tear.
Scale: For hobbyist or small-scale projects, small-scale jaw crushers might be available, though they are primarily industrial machines. For industrial 3D printing applications (e.g., large-scale additive construction using basalt-based concrete), a full production line is required.
Companies like Rubble Master, Zoneding Machine, and FTM Machinery manufacture industrial basalt processing equipment, and platforms like Alibaba.com list a variety of crushers and mills
Its been quite awhile since I posted the rovers and lander information to this topic Mars weather reporting
As GW noted possibly part of the reason that the mole failed to reach depth.
A vertical farming greenhouse hydroponic system integrates stacked growing structures (like towers or shelves) with soilless hydroponics inside a controlled greenhouse, maximizing yield per square foot by growing upwards, using nutrient-rich water to feed roots for high efficiency, reduced water use, and minimal pesticide needs, creating ideal microclimates for crops like leafy greens and herbs year-round.
How it Works:
Vertical Structures: Plants are grown on stacked layers or in towers, rather than just flat fields, increasing planting density.
Hydroponics: A nutrient-rich water solution (instead of soil) delivers essential minerals directly to the plant roots, often via a closed-loop system where excess water is recycled.
Greenhouse Environment: The structure controls light (supplemented by LEDs), temperature, humidity, and CO2, creating optimal conditions and protecting plants from pests and weather.
Aeroponics (Optional): Some systems mist roots directly with nutrients, offering even better oxygen access.Key Benefits:
High Yields: Significantly more food from less space (e.g., an acre of vertical farming can equal 40 acres of traditional farming).
Water Efficiency: Uses drastically less water (up to 95% less) due to recirculation.
Pesticide Reduction: Enclosed environment minimizes pests and pathogens, reducing or eliminating pesticide reliance.
Year-Round Production: Climate control enables consistent harvests regardless of external seasons.
Common Crops:
Leafy greens (lettuce, spinach, kale)
Herbs (basil, mint, cilantro)
Strawberries, small fruiting crops
Considerations:
High Initial Cost: Specialized equipment and technology require significant investment.
Energy Use: Can be energy-intensive for lighting and HVAC, requiring efficient systems.
Technical Knowledge: Requires expertise in controlled environment agriculture (CEA).For Mars, vertical farming greenhouses using hydroponics are key for life support, relying on enclosed systems (like inflatable units or stacked modules) for soil-free growth, recycling water/waste, and providing oxygen, food (greens, superfoods), and air revitalization, using LEDs for light and Nutrient Film Technique (NFT) or Dutch Buckets for efficient water/nutrient delivery, creating compact, high-yield farms vital for sustainable long-duration missions.
Key Technologies & Concepts:
Hydroponics: Growing plants without soil, using nutrient-rich water solutions (NFT, Dutch Buckets) to deliver precise nutrients to roots, drastically reducing water use.
Vertical Farming: Stacking plants in layers, maximizing crop production in minimal space, ideal for confined habitats.
Bioregenerative Life Support (BLSS): Integrated systems that use plants to produce food, oxygen, and recycle waste (water, human/plant waste), essential for closed-loop sustainability.
Greenhouse Structures: Inflatable cylindrical units (like the Lunar Greenhouse prototype) or modular, stacked cubes (like NUCLEUS) provide controlled environments.
Lighting: LEDs provide energy-efficient, tunable light, often with specific wavelengths (like purple hues) to optimize plant growth, mimicking or supplementing Martian sunlight.
Mars-Specific Adaptations: Systems are designed for low gravity/pressure, using sealed environments, Mars-like day length (a "sol"), and potentially using processed Martian resources.
Examples & Research:
NASA's MLGH: An inflatable hydroponic system using Cable-Culture (NFT variant) for astronauts' food, air, and water.
Project HOME (Embry-Riddle): Focuses on "superfoods" (Moringa, kale, etc.) in hydroponics under Mars light conditions, testing nutrient sufficiency.
Interstellar Lab's NUCLEUS: Modular pods for growing various crops and even insects for a full diet.
Benefits for Mars:
Food Security: Fresh, nutritious food (vitamins, minerals, fiber) for long missions.
Resource Efficiency: Extreme water savings, efficient nutrient use, waste recycling.
Environmental Control: Provides oxygen, removes CO2, recycles water, crucial for life support.
Space Efficiency: Vertical stacking maximizes yield in limited habitat volume.
Thermo syphon is the process that uses no pumps.
A thermosyphon cooling system uses natural convection (hot fluid rises, cold fluid sinks) to circulate a coolant (like water or oil) for passive, pump-free heat removal, relying on gravity and density changes to create a continuous flow from a heat source to a radiator or heat sink and back. Common in early cars (Ford Model T), modern electronics, and solar water heaters, it's simple, reliable, and energy-efficient but best for lower heat loads where the radiator sits above the heat source.
How it Works (Engine Example)
Heat Absorption: Water in the engine's water jacket absorbs heat from the cylinders.
Rising Hot Water: The heated water becomes less dense and rises through an upper hose to the radiator's top tank.
Cooling in Radiator: Air passing over the radiator fins (often aided by a fan) cools the water as it flows down through the tubes.
Sinking Cold Water: The now cooler, denser water sinks to the radiator's bottom tank and returns to the engine via a lower hose, completing the cycle.
Key Principles & Components
Natural Convection: Relies on the difference in density between hot and cold fluids.
Gravity: The radiator must be positioned higher than the heat source for gravity to assist flow.
No Pump: Eliminates the need for a mechanical water pump, saving energy and reducing complexity.
Heat Exchanger: A radiator or cooling coils dissipate heat into the surrounding air or another cooling medium.
Applications
Automotive: Older cars (e.g., Ford Model T) and some small engines.
Electronics: Cooling CPUs and power modules in servers, telecom base stations, and control panels.
Solar: Solar water heaters use thermosiphons to circulate water.
Industrial: Cooling mechanical seals in pumps.Advantages & Limitations
Pros: Simple, reliable, low maintenance, no extra energy input needed.
Cons: Less efficient for high heat loads; requires specific vertical positioning (radiator above engine/heat source)
https://thespoon.tech/the-mars-farm-a-n … t-reality/
Vertical Farming is due to energy costs...
Equipment costs
Real-estate costs and taxes
Employment costs
Middleman cut for getting it to market
The Future of Agriculture: Designing Tomorrow-1
The Future of Agriculture: Soilless Agriculture-2
The Future of Agriculture: Geodesic Domes-3
Ya I remember Steve only wanted to post his paper Proposal: Storing Energy, Introducing a "Cell", a Soil Factory on Mars that missed many issues like all projects geared to mars.
1. Assumed starting point magically happens with no build up of equipment or facts for mars to support doing it.
2. Thinking that burning the insitu from produced fuels and oxygen is a good thing for heat when a NUCLEAR REACTOR in any form requires heat removal that can be used.
3. Starter soil manufacturing to fill the trays only glances at the issue
4. full atmospheric pressure of earth within the structure.
All which I tried to bring up and more, once I move all of my posts Companion: Storing Energy, Introducing a "Cell", a Soil Factory .
The topic has been edited and updated but still contains errors.
Looking at this image suggests Vertical Farming and Indoor farming update


Food for Thought, what does a garden need to grow
Contains the ISS foods which are sent aprox 200 types
However, the team found that the main experiment yielded fewer fruits than expected. Palmer says that this is due to the challenges of getting the light, temperature and irrigation just right in larger growing spaces.
That is the nature of the starting of the parabolic shape but that's as far as it goes.
Adaptive dome lighting for day / night simulation can be directly powered by solar panels to follow mars sol cycle.
Of course cleaning system will be needed for the panels to keep full power coming out of them but that off loads power from the other systems. Chose bulbs that come on from a DC source voltage and they will follow as power ramps up and down. Between the storage battery and the lights the power is processed through a pulse width modulation and current circuit before powering the lights.
Designing a Martian menu involves creating a sustainable food system that provides nutritious, tasty, and varied meals with minimal resources for years, focusing on lightweight, shelf-stable items (like freeze-dried foods) and on-site crop growth (e.g., potatoes, spirulina, lettuce) to combat menu fatigue, ensure health, and support crew morale far from Earth, addressing major challenges like water usage, waste, energy, and microgravity cooking.
Key Components of a Martian Food System:
Pre-Packaged & Processed Foods:
Freeze-dried/Dehydrated: Water is removed to reduce weight and extend shelf life, requiring rehydration with water. Examples: fruits, vegetables, meats.
Thermostabilized: Similar to Earth canned/pouch foods, sealed for preservation.
Natural/Semi-Dried: Ready-to-eat items.
Condiments: Sauces, spices to add flavor variety.
On-Site Production ( Hydroponics/Aeroponics): Growing crops like potatoes, tomatoes, soybeans, wheat, spinach, lettuce, and nutrient-rich spirulina (algae).
Cellular Agriculture: Culturing meat or other proteins (future potential).
Menu Design Principles:
Nutrition: Meet daily caloric needs, maintain nutrient density over years, support bone/muscle health in low gravity.
Palatability & Variety: Combat menu fatigue with diverse flavors, textures, and easy preparation to keep astronauts eating well.
Resource Efficiency: Minimize mass, volume, energy, and water use; reduce waste.
Safety: Rigorous testing for contaminants in closed-loop systems.
Simplicity: Quick, easy meal prep for busy schedules in microgravity.
Sample "Martian" Meal Ideas:
Breakfast: Freeze-dried berries with rehydrated yogurt, wheat porridge with spirulina boost, or omelets with hydroponic spinach.
Lunch: Tomato soup (from dried tomatoes) with soy-based protein, sandwiches on Martian-grown wheat bread, or spirulina-enriched pasta.
Dinner: Rehydrated chicken/beef with freeze-dried veggies, potato-based dishes, or "Martian" pizza using grown ingredients.
Key Challenges Addressed by the Menu:
Transportation Costs: Freeze-drying reduces weight, making food cheaper to launch.
Psychological Support: Familiar, tasty food improves crew well-being.
Sustainability: Growing food on Mars creates a closed-loop system, reducing Earth reliance
The Menu for Mars: Designing a Deep Space Food System
The Nutrition paper, authored by NASA scientists Douglas, Sara Zwart, and Scott Smith, highlights the general criteria for a potential Mars or other space exploration mission food system, including:
Safety: The space station’s food system is tested and processed on Earth to ensure the food is safe for astronauts to eat. Food grown aboard the spacecraft and in microgravity could interact with microbes that float and mix with the spacecraft’s atmosphere until removed by air and water filters. Thus, resources will be required for cleaning and testing to reduce the risk of crews succumbing to foodborne illnesses.
Stability: Crews will not have the luxury of phoning home to resupply food on a multi-year, round-trip mission to Mars, meaning the food that the crew members bring with them or grow must last for years. Consequently, the nutrition and quality of the Mars food system must be stable for the length of the mission.
Palatability: Equally important is ensuring the food on a Mars mission is enjoyable to consume. Otherwise, astronauts may not consume enough food to support their health and well-being.
Nutrition: The Mars food system must provide food that is as nutritious as it is delicious. To function, the human body requires a handful of essential nutrients that must be absorbed from food. Failing to fulfill any one of these nutritional requirements can result in a deficiency that leads to a variety of health problems.
Resource minimization: Resources such as water, power, and volume are limited in a spacecraft. The Mars food system needs to provide safe, nutritious, palatable food while keeping resource consumption and waste production to a minimum. “You can have a food system that provides everything you need, but if it doesn’t fit within the resources, you cannot take it with you,” Douglas said.
Variety: The Mars food system must provide a variety of food so that astronauts don’t grow tired of consuming the same thing. “Menu fatigue” can dampen crew morale and cause astronauts to eat less, which can lead to health issues.
Reliability: “One of the big concerns with growing food is that if it doesn’t grow and you were depending on it, now you have insufficient food, which can be a very, very big concern when you’re going on these missions,” Douglas said. As a result, an exploration mission food system has to be dependable.
Usability: The Mars food system must allow crews to prepare meals with ease, providing them the time to focus on mission-critical tasks. “Prepackaged foods are a great candidate because they are easy to prepare, easy to consume. They already have a safe and long history in spaceflight, but there are some challenges with them—that nutrition and quality degrade over time,” Douglas said. “So, on longer missions, it would be nice to get a fresh component.”
Space-ready appliances: Astronauts aboard the space station prepare meals with heat or by adding water. The Mars food system will require new food preparation equipment that satisfies safety and spaceflight requirements.
Key Takeaway: If Earth engineers can manage the air quality for 76,000 people in that volume, we can certainly manage the "internal weather" for our proposed village.
The air volume inside the Caesars Superdome (formerly Louisiana Superdome) is a massive quantity, often cited as over 125 million cubic feet or sometimes specified as around 2.4 x 10^6 m³ (2.4 million cubic meters), encompassing the entire vast interior space, which is cooled by a huge 9,000-ton air conditioning system.
Key Figures:
Volume: ~125 million cubic feet (or ~2.4 million cubic meters).
Cooling Capacity: 9,000 tons of air conditioning.
Area: The arena floor alone offers 166,180 square feet (3.8 acres).
This vast space, designed to hold tens of thousands of fans, requires a significant cooling system to maintain comfortable temperatures
That is an air exchanger system that uses the total earth atmosphere for the exchanging source. Mars doe not have that.
post 4 greenhouse is sized for 1 crewman's life support of food and recycling of waste as well as air. The approximate 5.5 m long cylinder is about 2 m diameter. That means roughly 20 m^3 making use of vertical height and not just surface area. But I think we should double that as the aliases in the middle of the example'
The greenhouse is to support 50% of food with 100% for water and Oxygen for the original size.
If just half of the dome 31,000 m^3 is used for the life support that means we have a max number of crew that it can support just 440 crew when habitat area for them is based on 140m^3 that crews of 4 will make use of.
Floor to ceiling areas require all of the plumbing, vents for heating and cooling plus, water and waste removal and electrical with in a distance of 1.5 meter for each floor. planned in post 15 with the diameter is half of the dome distance at that height.
Using LED's we need just for light even using just 20w units to give 500 lumens or what is a 100w incandescent bulbs amount. Groups that need higher levels would have greater bulb density.
440 x 20w = 8.8k w x 25hr = 220kwhr daily consumed if we waste the power by having them all on.
Some plants want less and some more so post 13 is why we have varying intensities.
So until a crop plot area is planted the amounts are minimum with ability to go up in intensity.
With current prepackaged foods designed for space, six crew members living on Mars for 1,095 days will require over 13 tons (12,023 kilograms) of food.
Concrete, rebar and steel girder trusses is not viable until equipment for smelting and other foundry equipment is present. The structure is a temporary use and does not count that we need a supply system that mars does not have.
post for the dome
The dome shown here has a diameter of 200m (650'). This gives an internal land area of 3.14 hectares.
I am reminded of Biosphere 2 size and scale.
https://en.wikipedia.org/wiki/Biosphere_2
It is a 3.14-acre (1.27-hectare)[2] structure originally built to be an artificial, materially closed ecological system, or vivarium.
The main Biosphere 2 crew size for its primary two-year mission (1991-1993) was eight people (four men, four women) in a sealed, self-sustaining ecosystem, with a smaller, seven-person crew for a shorter, second mission in 1994. These crews studied closed-system living, a precursor to space colonization, managing complex biomes and food production within the massive glass structure.
seven biome areas were a 1,900-square-meter (20,000 sq ft) rainforest, an 850-square-meter (9,100 sq ft) ocean with a coral reef, a 450-square-meter (4,800 sq ft) mangrove wetlands, a 1,300-square-metre (14,000 sq ft) savannah grassland, a 1,400-square-meter (15,000 sq ft) fog desert, and two anthropogenic biomes: a 2,500-square-meter (27,000 sq ft) agricultural system and a human habitat with living spaces, laboratories and workshops.
The oxygen inside the facility, which began at 20.9%, fell at a steady pace and after 16 months was down to 14.5%. This is equivalent to the oxygen availability at an elevation of 4,080 meters (13,390 ft
Lets not repeat failure by assuming earth as the base.
The lunar mars greenhouse is sized for 5.5m by 2.1 meter cylinder that used a 1000 w mercury light for heat as well as for light. Something that we will not be doing.
For a single astronaut, a lunar greenhouse needs enough space for food, air, and water recycling, with NASA concepts suggesting around 28-40 square meters (300-430 sq ft) of cultivation area for 50% caloric needs, while smaller habitat modules might use 3-4.5 m² for basic needs, emphasizing volume and flexibility, not just area, for crew comfort and functions. Actual sizes vary wildly, from small, deployable units to massive, buried structures, but expect a dedicated module or significant habitat volume.
Key Factors Influencing Size:Food vs. Life Support: A greenhouse providing 100% oxygen and water recycling needs a different footprint than one just supplementing food.
Caloric Needs: Growing 50% of a 2000 kcal/day diet (1000 kcal) requires roughly 28-40 m².
Habitat Integration: Some designs integrate growing areas within living quarters (like HAVEN), while others are separate, buried modules for radiation protection.Technology: Hydroponics, lighting, and automation affect space efficiency.
Examples of Proposed Sizes:
ED&EN ISS Prototype: Around 30 m² (323 sq ft) for food on Moon/Mars.
Mars-Lunar Greenhouse (MLGH): Aims for 28-40 m² for a crew of four.
Lunar FARM (Concept): A large concept with 538 m² for 18 astronauts, showing scalability.
HAVEN (Habitat Module): Smaller modules (3-4.5 m²) offer storage and basic functions, with larger crew quarters for standing/moving.In Summary for One Person:
You're likely looking at a dedicated space of at least 30 square meters for significant food and life support, or a smaller, integrated volume within a habitat for basic functions, emphasizing efficiency and multi-use areas
MARS GREENHOUSES: CONCEPTS AND CHALLENGES
Proceedings from a 1999 Workshop
tahanson43206 wrote:For SpaceNut ...
Nice image in https://newmars.com/forums/viewtopic.ph … 86#p236186
Please see if your AI Friend is capable of doing more than just offering hand waving and high level overviews.
We need specific equipment recommendations for Calliban's Dome.
GW Johnson is (currently) thinking about cooling air and removing water by creating an opening from the dome for passage of air to outside radiators. I am worried that precious thermal energy would be lost to the dome interior if that were done.
I think your illustration of a mechanism inside the dome has the opportunity to avoid loss of thermal energy to Mars.
Please see if your AI friend can recommend specific off-the-shelf products to handle the air inside Calliban's Dome.
Also... please consider going back to Calliban's original sketch of what the floor plan might look like. I think we've allowed ourselves to be distracted by the ideas of tiers of layers of housing. I know that Calliban introduced that idea, but I don't think we should give up on the Italian Plaza vision that Calliban showed us early on.
If we return to the Italian Plaza vision, then we are creating something that wealthy Martians can inhabit, and working Martians can visit for special occasions.
(th)
A each structure need room sizes and more to get near to the foot print of light and power requirement for the number of crew it is meant to sustain.
High level view is also needed for the crop growth until you define the limits of oxygen from the crops, the types of crops the foot print of the greenhouse size ect...
We know that outside conduction via a working fluid that does not freeze is the means for dome cooling but that still need a flow rate and exchange to get to the pump size and power levels.