LUNAR MASS DRIVER SIMULATOR
LUNAR + POWER INTEGRATION sovereignagentics.io
Lunar Mass Driver Simulator
Full lunar electromagnetic launcher sim + He³ Mining + Export module. Power from solar tools, trajectory, energy recovery, launch cadence + high-value ³He regolith export economics. Scale the power foundation into real lunar industry.

Simulator Inputs

HE³ MINING + EXPORT MODULE — high value lunar stream
He³ ~ppb in regolith. Mining + sep + MD export power overhead modeled. Revenue offsets power infrastructure costs. Fresnel Solar (60-75% eff, Low mass) vs MW/Laser per table.

Simulation Results

TRACK + PAYLOAD ANIMATION
POWER DEMAND vs SOLAR (lunar day cycle)

About the Lunar Mass Driver Simulator

A mass driver is an electromagnetic catapult that accelerates payloads off the Moon without rockets, trading propellant for electricity. This simulator models the achievable exit velocity, the energy per launch, how much of that energy can be recovered, and how many launches per day a given power system supports.

Because the Moon has no atmosphere and low gravity, electromagnetic launch is unusually attractive there — and this tool quantifies just how attractive under your assumptions.

How to use it

  1. Set the available solar power and the share allocated to launch.
  2. Configure the driver's performance parameters.
  3. Run the simulation to read exit velocity, MWh per launch, and recovered energy.
  4. See peak power, launches possible per day, and the implied helium-3 or cargo export cadence.

How it works

Kinetic energy rises with the square of exit velocity, so reaching lunar-escape or transfer speeds demands a large energy pulse per shot. The simulator computes that per-launch energy, subtracts what regenerative braking can recover, and divides your launch-power budget by the net demand to get daily cadence.

It also surfaces peak power, which often sizes the capacitor bank or flywheel rather than average power — a distinction that dominates real mass-driver design and is easy to miss without a model.

Worked example

Sending payloads to low lunar orbit needs a few kilometres per second and a sizeable megawatt-hour pulse each shot; with tens of megawatts allocated and partial energy recovery, the driver supports a steady handful of launches per day — enough to bootstrap an export economy.

Frequently asked questions

Why a mass driver instead of rockets?

It uses electricity, not propellant, which is compelling on the airless, low-gravity Moon where solar power is abundant.

What limits launches per day?

Net energy per launch versus your power budget, and peak-power handling for each pulse.

Does energy recovery matter?

Yes — recovering part of each launch's energy meaningfully raises cadence, and the model lets you vary it.

Is this design-grade?

No — it is an educational first-order estimator with open assumptions.

Offline and translated?

Yes — browser-only and available in 25 languages.

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