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Design blueprint derived from the source paper (DOI 10.5281/zenodo.24180128): This paper computes a laser ablation shepherd that delivers 12,000 W of optical power onto a 110 m asteroid of mass 1,672,583,929 kg. With an ablation energy of 8,000,000 J per kilogram and an ejecta speed of 1,100 m per second, the vaporised mass flow of 0.000825 kg per second produces 0.908 N of recoil thrust and an acceleration of 5.43e-10 m per second squared. Over 2 years the system delivers 34.2 mm per second against a requirement of 22.6 mm per second, a margin ratio of 1.51, a computed separation of 10,591 km, and a total ablated mass of 52,070 kg. This is a computed study of a deflection system for planetary defence, with no targeting or weapon application. It is simulated, not measured. Status: DESIGN BLUEPRINT — SIMULATED, NOT MEASURED — NOT BUILT. All numbers are simulated values from the source paper's computation, deposited with this blueprint as compute.py and results.json. AI-use disclosure: Dave, an AI research system, assisted with the computation and drafting under the author's direction; author of record William Alexander Aldred.
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William Alexander Aldred (2026) studied this question.
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