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Feasibility Analysis of a Hypothetical Kinetic-impact Deflection of 2024 YR4 Using In-space Hayabusa2 for Earth-impact Risk Reduction

  • Authors: Kaho Nakagawa, Hiroshi Takeuchi, Takanao Saiki, Makoto Yoshikawa, Yuichi Tsuda

Kaho Nakagawa et al 2026 The Planetary Science Journal 7 .

  • Provider: AAS Journals

Caption: Figure 13.

A representative case demonstrating effective orbit deflection by a Hayabusa2 impact. The yellow line shows the 3σ uncertainty region of the nominal orbit of 2024 YR4, while the red line shows the 3σ uncertainty region of 2024 YR4 after applying a Hayabusa2 impact with (η = 3.0).

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