Numerical optimization of low-thrust trajectories shows TNOs can reach Mars-impacting orbits with ΔV of 2.5–3.2 km/s over 380–540 years, with further savings from a Neptune flyby.
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Energetic Feasibility of Redirecting Trans-Neptunian Objects onto Mars-Impacting Orbits: Continuous Thrust and Gravity Assist Trajectories
Numerical optimization of low-thrust trajectories shows TNOs can reach Mars-impacting orbits with ΔV of 2.5–3.2 km/s over 380–540 years, with further savings from a Neptune flyby.