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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 6.

Approach trajectory in a coordinate system with the Sun and 2024 YR4 fixed. The coordinate system has the X-axis pointing from the Sun toward 2024 YR4 and the Z-axis aligned with the direction of 2024 YR4’s orbital angular momentum. The Y-axis corresponds to the approximate direction of 2024 YR4’s orbital velocity. In Case 1 (left), Hayabusa2 approaches 2024 YR4 from the sunward side, whereas in Case 2 (right), it approaches from the antisolar side.

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