Pre-seed · Robotics, Physical AI & AI Infrastructure

The autonomy that sets the cost of lunar helium-3

Ithil decides where to dig, and keeps machines digging where no one can repair them.

Benjamin Lee, Founder  ·  ithilenergy.io

Why now

AI needs clean, firm power faster than the grid can deliver it

Global data-center electricity, TWh

2024: 415 TWh 2030: ~945 TWh 415 ~945 2024 2030 2.3×

+17%

Data-center electricity growth in 2025

200 MW

Google's fusion offtake with Commonwealth Fusion (2025). Microsoft signed with Helion in 2023.

19

NASA lunar landings planned for 2027 and 2028

Sources: IEA, Energy and AI (base case); company announcements; NASA CLPS manifest

The fuel

Helium-3 is the cleanest fusion fuel. It costs 20× too much.

Price per kilogram of helium-3

Today

Earth supply

$20M

What fusion can pay

To compete as fuel

$1M

88 GWh

Electricity from one kilogram

Few neutrons

A fraction of what deuterium-tritium fuel releases

Sources: DOE National Isotope Development Center; market pricing

The supply

Earth makes 3–4 kg a year. 2030's data centers alone would need 11,000.

One dot: Earth's entire annual supply, ~3.5 kg

The whole grid: helium-3 for 2030 data-center demand, ~11 t a year

0.7–1.7 Mt

Estimated helium-3 on the Moon, deposited by solar wind over billions of years

~11 t = IEA 2030 data-center demand (~945 TWh) ÷ 88 GWh per kg

The problem

Every kilogram means moving 100,000 tonnes of lunar soil

At 4–15 parts per billion, cost per kilogram is set by two things nobody has solved.

01

Finding the richest ground

Grade varies several-fold from site to site and has never been measured on the Moon itself. Every dig in the wrong place burns power and machine life.

02

Keeping machines working

No humans, abrasive dust, 14-day nights and a signal delay. No excavator has ever operated there. Apollo's seals failed after two EVAs; a commercial plant needs 5,000 hours.

Both are AI and robotics problems.

The solution

Ithil decides where to dig, and keeps the machines digging

Vendor-neutral autonomy software. It runs on anyone's excavator, rover or processing plant.

Find the richest ground

Orbital titanium and solar-wind maps fused with rover samples into a grade map with uncertainty. Active learning picks the next sample site.

Keep machines working

Remaining life estimated from force, current, vibration and thermal telemetry. Faults recovered on board. Work scheduled around the 14-day night.

Optimize both at once

The richest ground is often the rockiest and furthest from power. Ithil trades grade against wear and energy to maximize kilograms over the fleet's life.

Product

One planner for grade, wear and power

Orbital mapsTitanium, soil maturity
Rover samplesIn-situ grade
Machine telemetryForce, current, thermal
Grade modelMap with uncertainty
Wear modelRemaining useful life
Joint plannerMaximizes kilograms over the fleet's life, within the power and thermal budget
Dig
Haul
Process
Idle

Runs on
NASA's cFS and F Prime flight frameworks. Ithil sits on top; it doesn't replace them.

Learns
From Earth fleets first. Every processed batch becomes a ground-truth grade measurement.

The technical core

The hard part: learning without breaking machines

Formally, constrained stochastic control over a mixed fleet, where each machine's wear is hidden, irreversible and depends on how it's run.

Wear can't be measured, only inferred

Remaining life is estimated from force, current, vibration and thermal telemetry, a prognostics problem with training data on Earth.

The wear model changes by site

Tool–soil interaction in low gravity is poorly characterized, so the controller adapts online instead of running fixed gains.

Failure can't be explored

Failure is permanent and fleets are tiny. That rules out standard reinforcement learning: we use conservative policy improvement.

Open-loop digs; it doesn't optimize

Open-loop control is enough for site preparation. It can't trade output against remaining life under a power cap.

Market

Budgets for this autonomy exist today. The fuel market is the prize.

TAM · annual, 2030s

$10B+

Helium-3 fuel for 2030's data-center demand: ~11 t a year at a fusion-viable ~$1M/kg

SAM · programs buying it now

$20B

NASA Moon Base program (total)

$2B+

Nuclear-decommissioning robotics on Earth

SOM · year-3 revenue target

[$__]

[__] machines under license plus [__] operations contracts

TAM is annual; SAM figures are program totals. Sources: IEA; NASA

Competition

Everyone else optimizes one machine or one fleet

Vendor-neutralPicks sites by gradePlans for wearBuilt for the Moon
IthilYesYesYesYes
Interlune, with VermeerNo, own fleetOwn sitesNot publicYes
Magna PetraNo, own hardwareNot publicNot publicYes
Pronto, ASI Mining (retrofit)YesNo, haulageNot publicNo
OEM autonomy (Cat, Komatsu)No, own fleetNoNot publicNo

Moat: neutrality plus cross-fleet wear data that no single vendor can collect. NASA's cFS and F Prime aren't competitors; Ithil runs on them.

Ithil's capabilities are designed, not yet built. Competitor entries from public information.

Business model

Software revenue first. A royalty on every kilogram later.

From 2026

Software license

Per machine, per year, on any vendor's hardware.

[$__ per machine-year]

From 2027

Operations contracts

Per mission on the Moon, per site on Earth: planning, monitoring and model updates.

2030+

Production royalty

Per kilogram extracted, once operators are producing helium-3.

Software margins from day one: [target gross margin __%]. Early revenue doesn't depend on helium-3 production.

Go-to-market

Earth first, then the Moon

Now – 2027

Earth pilots

Paid pilots in nuclear decommissioning and mining: revenue plus the wear and energy data the models need.

Design partner: [Name]

2027 – 2029

Lunar missions

Fly on NASA Moon Base and CLPS missions through hardware partners. NASA SBIR/STTR funds early work.

2030+

Lunar extraction

License plus royalty with helium-3 operators as production scales.

Channel: sold through hardware makers as their autonomy layer, and directly to mission operators.

Traction

The system is already architected

Designed as a Johns Hopkins systems engineering project, with design feedback from lunar hardware engineers.

  • HERMES: a full model-based systems engineering architecture for a helium-3 extraction plant, in SysML
  • Requirements traced to verification, including 5,000-hour operation and fault detection in under 5 s
  • Trade studies, interface definitions, risk register and test plan

Design feedback from

Kris Zacny, Honeybee Robotics
Dr. George Sowers, Colorado School of Mines
A former Blue Origin architect

Next build

[e.g. wear estimator trained on public excavator telemetry, run on a DEM regolith simulation]

Team

Benjamin Lee, Founder

Systems engineer and data scientist. Ithil's two problems are a decision under uncertainty and a reliability problem. He has shipped both.

Reliability from telemetry

Built telemetry and reliability analytics for Microsoft Copilot at production scale.

Decisions under uncertainty

Pricing and revenue optimization with statistical models.

The system, designed

Johns Hopkins M.S. in Systems Engineering; designed HERMES end to end.

Hiring next

Founding robotics and controls engineer with field-autonomy experience. [Name]

Financials

Three-year plan

RevenueCustomersHeadcountNet burn
Year 1[$__][__] pilots[__][$__]
Year 2[$__][__][__][$__]
Year 3[$__][__][__][$__]

Runway: [__] months on this raise. Non-dilutive: [NASA SBIR/STTR applications, if any]

The ask

Raising [$__] pre-seed

To build vendor-neutral autonomy for lunar extraction, starting on Earth.

Use of funds

  • Engineering, incl. robotics and controls hire[__%]
  • Simulation and bench rig[__%]
  • Pilots and partnerships[__%]

18-month milestones

  • Wear estimator validated on Earth fleet data
  • First paid Earth pilot
  • NASA SBIR award or hardware-partner LOI

Contact · [email]  ·  ithilenergy.io

Appendix · Energy check

Extraction uses under 1% of the energy the fuel returns

Energy per kilogram of helium-3

Out

Electricity from fusion

88 GWh

In

Process heat, 85% recovered

~0.7 GWh

Source: University of Wisconsin Fusion Technology Institute, Mark II/III lunar miner design (heat to 700 °C, 85% recuperation)

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