ARLO / ACTIVE SHIELDING / CONCEPT RESEARCH

Make protection measurable.

A staged validation plan for magnetic radiation shielding and MatterVolt surface concepts, from baseline models to independent review.

Explore the research ↓
Concept visualization · not a field solution or built hardware
Current evidenceLiterature + analytical modelNo measured ARLO shielding benefit
01

Gate 1 — freeze the comparison

Record orbit, geometry, material inventory, spectra, scoring volumes and mission duration. Include a no-field case and a passive-only case at equal installed mass. Predeclare success and stop criteria before searching for an attractive geometry.

02

Gate 2 — verify field and particle calculations

Check field solvers against analytic coil cases and measured maps. Check trajectory integration against a uniform-field helix and demonstrate convergence with step size. Include relativistic momentum where necessary. Cross-check representative cases using an independent implementation.

03

Gate 3 — calculate dose, not just deflection

Use a validated radiation transport framework to account for interactions in coils, supports and station materials, including secondaries. Report uncertainty and locations where dose increases as well as decreases. A particle animation or magnetic-rigidity calculator cannot close this gate.

04

Gate 4 — separate the physical experiments

Measure field topology and particle deflection with a controlled source and calibrated detectors at a suitable test facility. Test optical and thermal coupons separately. A low-energy beam demonstration does not validate cosmic-ray protection; declare exactly which species and energy range each test covers.

05

Gate 5 — close the installed system

Compare thermal, electrical, structural and failure budgets with the baseline. Require external technical review before an uncrewed demonstrator is considered. Crew safety must not depend on experimental shielding. Present status: literature-grounded concept and analytical teaching tool; no shield prototype, radiation-transport result or measured ARLO dose benefit.

Research foundations

External work informs the study; it does not validate ARLO. Review date: 24 October 2026. Source access depth is stated below.

  1. NASA MAARSS engineering study, 2019 ↗

    Architecture, structural loads, quench protection and cooling; report summary reviewed.

  2. CREW HaT, Desiati & D’Onghia, 2022 ↗

    Preliminary magnetic habitat concept; abstract reviewed, not flight validation.

  3. Hesse-Withbroe & Arquilla, 2025 ↗

    Modeling preprint; revised strong-field performance. Abstract reviewed.

  4. NASA LEO station radiation environment, 2024 ↗

    Orbit-specific environment reference; presentation.

  5. NASA thermal-control overview ↗

    Engineering context for coatings, heat rejection and environment.

  6. ESA spacecraft impact shielding ↗

    Physical debris protection remains a separate system.

  7. NASA spacecraft power systems ↗

    Solar generation, eclipse storage and end-of-life considerations; overview reviewed.

FOLLOW THE DESIGN

Explore the next question.

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Help test the protection concept.

We are defining a research scope for radiation transport, superconducting engineering and optical-material testing. No shield is offered for sale or operational use.

Discuss a technical contribution ↗Return to ARLO ↗