Non-Nuclear Inertial-Thermal Energy System for Deep Space Missions

This technical paper presents a verified, non-nuclear energy generation system designed for long-duration, low-power deep space missions. It details an Inconel 718 flywheel architecture with integrated electromagnetic and thermoelectric energy recovery subsystems. All components are based on proven aerospace materials and methods. The system offers a regulatory-safe alternative to RTGs, with applications in outer solar system sensors, data relays, and CubeSat missions.

Publication Details

Journal
Zenodo (CERN European Organization for Nuclear Research)
Published
2025-07-12
DOI
https://doi.org/10.5281/zenodo.15869494
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
0.00
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article

Non-Nuclear Inertial-Thermal Energy System for Deep Space Missions

Zenodo (CERN European Organization for Nuclear Research)
Spacecraft Design and Technology
article

Non-Nuclear Inertial-Thermal Energy System for Deep Space Missions

article en

Abstract

This technical paper presents a verified, non-nuclear energy generation system designed for long-duration, low-power deep space missions. It details an Inconel 718 flywheel architecture with integrated electromagnetic and thermoelectric energy recovery subsystems. All components are based on proven aerospace materials and methods. The system offers a regulatory-safe alternative to RTGs, with applications in outer solar system sensors, data relays, and CubeSat missions.

Zenodo (CERN European Organization for Nuclear Research)
Affordable and clean energy
Openalex Percentile: Top 41%
Spacecraft Design and Technology
DOIOpen Access PDFOpenAlex
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Non-Nuclear Inertial-Thermal Energy System for Deep Space Missions · Zenodo (CERN European Organization for Nuclear Research) (2025) | TGRS Research Map | TGRS