A Rotating Ring Habitat for Artificial Gravity: Radius, Rotation Rate, Structure and Shielded Core

This paper presents a computed design for a rotating ring that provides artificial gravity at its rim, with a non-rotating or counter-rotating shielded core for radiation refuge, sized from centripetal acceleration, rotation rate and hoop tension. The study is simulated, not measured. Using the stated assumptions in the Methods and the deposited calculation, the headline results are: omega = 0.572, rpm = 5.46, v = 17.2, period = 11.0, stress = 2, g_in = 0.93. All quantities are derived in the accompanying script, which writes the full numerical record to results.json, including inputs, outputs and, where relevant, a parameter sweep. The design is assessed on its computed performance, its mass and power budgets where relevant, and its failure behaviour. Where the computed result is impractical, that outcome is stated plainly in the abstract's terms as well as in the Discussion: the numbers, not the intention, decide whether the principle is attractive at the stated scale. No measurement of a built system is reported, and no flight performance is claimed.

Authors

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2026-11-11
DOI
https://doi.org/10.5281/zenodo.24145300
Citations
1
Primary Topic
Structural Analysis and Optimization
Type
article
Field-Weighted Citation Impact
1.89
Controls
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article

A Rotating Ring Habitat for Artificial Gravity: Radius, Rotation Rate, Structure and Shielded Core

William Alexander Aldred
1 citations
Zenodo (CERN European Organization for Nuclear Research)
Structural Analysis and Optimization
1.89
article

A Rotating Ring Habitat for Artificial Gravity: Radius, Rotation Rate, Structure and Shielded Core

William Alexander Aldred
article en
1 citations

Abstract

This paper presents a computed design for a rotating ring that provides artificial gravity at its rim, with a non-rotating or counter-rotating shielded core for radiation refuge, sized from centripetal acceleration, rotation rate and hoop tension. The study is simulated, not measured. Using the stated assumptions in the Methods and the deposited calculation, the headline results are: omega = 0.572, rpm = 5.46, v = 17.2, period = 11.0, stress = 2, g_in = 0.93. All quantities are derived in the accompanying script, which writes the full numerical record to results.json, including inputs, outputs and, where relevant, a parameter sweep. The design is assessed on its computed performance, its mass and power budgets where relevant, and its failure behaviour. Where the computed result is impractical, that outcome is stated plainly in the abstract's terms as well as in the Discussion: the numbers, not the intention, decide whether the principle is attractive at the stated scale. No measurement of a built system is reported, and no flight performance is claimed.

Zenodo (CERN European Organization for Nuclear Research)
Openalex Percentile: Top 21%
Structural Analysis and Optimization
1.89
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