INDEPENDENT PROPULSION RESEARCH

FIELDS.
FLOW.
FURTHER.

Can three magnetic sources transfer more momentum than one? Exploring plasma, field geometry, and the evidence a propulsion concept needs.

Open the PIC Observatory See the full spacecraft concept
SCROLL TO EXPLORECONCEPT → MODEL → EVIDENCE
PERFORMANCE REMAINS UNVALIDATED.
01 / THE RESEARCH QUESTION

THREE SOURCES.
ONE FAIR
COMPARISON.

A bigger magnetic footprint.
But does it do more?

DAIS studies how a flowing plasma interacts with magnetic sources. The primary hypothesis: a co-axial triad can transfer at least 10% more axial momentum than a single source at equal imposed magnetic-field resources.

The current work uses reduced-mass, two-dimensional electromagnetic particle-in-cell screening in WarpX. Reservoir stability comes first. Single-source convergence and a matched triad comparison follow only after the required gates pass.

Read the research briefs
[ 01 ]MATCH THE MAGNETIC RESOURCES.
[ 02 ]CLOSE THE ENERGY & MOMENTUM BUDGETS.
[ 03 ]VALIDATE BEFORE CLAIMING GAIN.
02 / THE FIELD CONCEPT ARTISTIC / INTERACTIVE

GIVE THE
FIELD A FORM.

Explore the geometry behind the question.
Then see how the actual tests are structured.
This model is an artistic interpretation.

DAIS / CONCEPT 01FIELD GEOMETRY
MAGNETIC TOPOLOGY / CONCEPT

Geometry is the question.

Explore an artistic propulsion assembly. The research compares a single source with a triad at equal imposed magnetic-field energy, then measures their momentum transfer.

64%
MINMAX

Concept visualization. Not a physics simulation or measured performance.

FROM THE CONCEPT TO THE TESTSEXPLORE THE PIC COMPARISON ↗
03 / THE RESEARCH PROGRAM

FOLLOW THE
EVIDENCE.

One primary comparison. An exploratory extension.
A validation protocol that keeps both accountable.

Research status · The stored reservoir gate remains unvalidated. No validated propulsion gain or mission-time prediction is established by this work.

3 research directions
04 / THE ARCHITECTURE CONCEPTHYPOTHESIS / NOT AN ENGINE DESIGN

A BIGGER
PICTURE.

The infographic imagines a flow-through spacecraft.
Beamed energy supplies power. External material supplies reaction mass. Each stage needs its own validation.

01 / ENERGY

Near-Sun power

Harvest solar energy and transmit a focused beam.

02 / RECEIVER

Beam reception

Convert received energy into usable spacecraft power.

03 / MATERIAL

Plasma collection

Collect external material and ionize it where needed.

04 / HYPOTHESIS

DAIS conditioning

Investigate whether controlled fields can organize the flow.

05 / ACCELERATION

Powered stages

Supply energy to accelerate the charged particles.

06 / EXHAUST

Magnetic nozzle

Direct the plasma exhaust and account for source reaction.

DAIS concept illustration: solar beamed power reaches a spacecraft receiver, followed by plasma collection, conditioning, acceleration and a magnetic nozzle. Other panels compare single and three-source magnetic fields, show a spacecraft cutaway, and list hypothetical results and travel times. See the text below for the research limitations.
Original research concept illustration. Its numerical gains and travel times are unverified claims, not results established by this repository.View full-size image ↗

The illustration sets a direction.
The research tests a smaller question.

The present PIC model addresses the single-source versus three-source interaction in panel 2. It does not simulate the receiver, collection, conditioning, powered acceleration, nozzle, or a mission trajectory. The image’s 2.03 gain and conditioning sweep numbers arrived without supporting code or data and are not calibration targets. Its faster Mars journeys remain hypothetical. Equal magnetic-field resources in the study must not be read as equal electrical power.

05 / THE VALIDATION PATHREPOSITORY SNAPSHOT / 27 SEP 2026

EVIDENCE
BEFORE GAIN.

A sequence of scientific prerequisites.
Missing evidence keeps the next comparison locked.

TEST 0 / NO MAGNET

Stabilize the reservoir.

Close particle and energy budgets. Check charge, local thermal variance, and drift across independent seeds and numerical refinements. Require at least ten flow crossings.

NOT VALIDATED

TEST 1 / SINGLE SOURCE

Establish the reference.

Freeze the passing reservoir. Demonstrate steady and converged momentum transfer to one source before using its impulse as the comparison denominator.

BLOCKED BY TEST 0

TEST 2 / THREE SOURCES

Measure the difference.

Compare matched source-field resources and physical intervals. Report the gain ratio with uncertainty. A point estimate of GR ≥ 1.10 alone cannot establish the claim.

COMPARISON NOT AUTHORIZED BY GATE

Static summary of the repository’s recorded state, not a live campaign feed. The observatory explains these steps and can inspect a saved JSON report locally.

Based on the project’s 2D kinetic study, locked TEST 0 protocol, stored reservoir gate, and DAIS-DYNAMIC development report. These public summaries accompany the concept; research source files and raw results are not part of this website.

THE NEXT STEP IS A BETTER TEST.

PLASMA. BOUNDARIES. EVIDENCE.

ENTER THE
EXPERIMENT.

Four ways to explore the physics. One standard of evidence.

Review the validation path
RESEARCH DIRECTION

Research brief

Explore the PIC tests

DAIS / PUBLIC RESEARCH SUMMARY · SEPTEMBER 2026