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Engineering analysis demonstrates a hardware-enforced authorization gate framework across safety-critical decision points in autonomous launch systems, suggesting a path for regulatory hazard...
This engineering preprint analyzes how a hardware-enforced human-authorization gate could be evaluated at safety-critical decision points in autonomous launch and re-entry systems. It uses 14 CFR §450.107 as the regulatory anchor for phase-specific hazard-control strategies, functional failures, safety-critical systems, and event timelines, and distinguishes the adjacent flight-abort requirements in §450.108. The paper proposes five candidate gate points and a falsifiable evaluation protocol. EHOX demonstrator measurements are reported separately from production or flight qualification claims. This document is not an FAA compliance determination, certification, or statement about SpaceX internal systems.
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Gerhard Hirschmann (2026) studied this question.
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