ARLO / ACTIVE SHIELDING / CONCEPT RESEARCH
Study candidate coil layouts, cryogenic loads, quench protection, docking access and passive shielding for ARLO.
Explore the research ↓Place a candidate coil arrangement around a limited crew refuge and compare it with a passive refuge of equal total installed mass. Examine all access directions, surrounding material and realistic occupancy. Concentrating protection is a study option, not a selected flight design.
Evaluate an external coil arrangement with a deliberately low-field occupied region, informed by published toroidal and Halbach-array concepts. Keep a conventional pressure vessel, debris protection and emergency systems. Coil geometry, current, standoff, conductor and temperature remain unresolved design variables.
Use a larger external array as a comparison case. Larger structures introduce launch packaging, deployment, flexibility, thermal and visiting-vehicle constraints. The first model should be allowed to reject this option; scale alone does not establish efficiency.
Superconducting operation still needs a controlled cold environment and current margin. Sum radiation, support conduction, current leads, joints and transient heat loads at the actual cold stage. Convert cold-stage load into spacecraft electrical demand using a specified cooler performance map. The nozzle’s heat-leak and coil-power figures cannot be scaled directly to this shield.
Use a structural model for magnetic loads and a fault model for quench detection, protection and energy discharge. Check loss of cooling, sensor failure and interrupted deployment. Evaluate fields and induced currents at docking vehicles, electronics, payloads and crew locations. NASA’s MAARSS work identifies these as coupled engineering issues [1].
External work informs the study; it does not validate ARLO. Review date: 24 October 2026. Source access depth is stated below.
Architecture, structural loads, quench protection and cooling; report summary reviewed.
Preliminary magnetic habitat concept; abstract reviewed, not flight validation.
Modeling preprint; revised strong-field performance. Abstract reviewed.
Orbit-specific environment reference; presentation.
Engineering context for coatings, heat rejection and environment.
Physical debris protection remains a separate system.
Solar generation, eclipse storage and end-of-life considerations; overview reviewed.
FOLLOW THE DESIGN
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 ↗