Lunar industrial infrastructure
LunarFoundry models the extraction, refining, power, and infrastructure plans needed to turn regolith into usable off-world supply—before you freeze mass to orbit.
Extraction nodes · oxygen, silicon, aluminum, iron, glass, regolith feedstock
The Moon cannot become infrastructure if every kilogram comes from Earth. These are the constraints mission teams hit first.
Launch and landing margins dominate lunar programs. If construction and propellant precursors ride uphill, timelines stretch and architectures shrink.
Aggregate, glassy phases, metals, and oxygen have to come from regolith—or you are building a logistics chain, not a surface economy.
Night survival, thermal swings, and process duty cycles set the real ceiling on tons per year—not slide-deck optimism.
Programs stall when teams cannot agree on yield envelopes, equipment mass, or what “pilot scale” actually implies for the grid.
Survey, pilot extraction, refining, storage, and export each carry different interfaces. Skip a phase and the next one fails in integration.
Model how much oxygen, metal, or glass a lunar site can produce before you design the mission around it. Select region, material, power architecture, extraction route, landed mass, duration, and objective—get yield, power, phases, economics, and risk in one pass.
Product preview · run live on /demo
Propellant / life-support precursor from regolith and polar volatile access patterns.
PV and electronics feedstock—linked to beneficiation and melt discipline.
Structural metal from anorthite-rich routes; ties to electrolysis and thermal budgets.
Reduction from ilmenite and oxide phases; anchor for tooling and magnetic beneficiation.
Agglutinate-driven glass for in-situ casting and binder pathways.
Sintered regolith and graded fill for roads, berms, and robotic construction lanes.
Orbital + surface truth for chemistry, thermal environment, and logistics corridors.
Throughput-prove the feed system and dust isolation at reduced duty.
Product qualification against habitat and fabrication contamination budgets.
Buffer tanks, silos, and thermal mass for night and peak shaving.
Packaging glass and aggregate for robotics and surface assembly.
Continuous production with maintenance loops sized for uncrewed intervals.
Resource yield forecast, power demand, equipment mass context, processing timeline, launch mass avoided, risk matrix, site suitability, phased infrastructure, material output cards, and mission economics—aligned to how lunar programs actually review trades.
Oxygen yield (example)
420 kg/month
Power demand (example)
82 kW
Launch mass avoided (example)
1,900 kg
Feasibility score (example)
74
Non-SaaS engagement models for serious lunar programs.
Region down-select, yield envelopes, power + landed mass sanity checks.
Integrated phases, risk matrix, and economics aligned to your launch cadence.
Pilot extraction + refining interface specs with robotics partners.
Multi-year planning office, data room, and joint roadmaps to scale.
Run the simulator, save missions to your dashboard, and bring a single artifact into your next program review.