AEROSPACE SHANGHAI, Volume. 41, Issue 6, 46(2024)
Potential Gain of Quasi-eccentric Collision on the Kinetic Impact Orbit Deflection in Planetary Defense Missions
Fig. 3.
Fig. 4. Thermodynamic diagrams of the velocity changes generated by each impact surface under three different attitudes when the interception angle is 5.22°
Fig. 5. Calculation process for a small celestial body kinetic energy impact mission
Fig. 7. Projection of the launch window of Apophis on the deflection distance-launch date plane
Fig. 8. Projection of the launch window of Apophis on the impact date-launch date plane
Fig. 10.
Fig. 11. Distribution of the deflection distance with 100 000 samples
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Kin Thong LEE, Zhaokui WANG. Potential Gain of Quasi-eccentric Collision on the Kinetic Impact Orbit Deflection in Planetary Defense Missions[J]. AEROSPACE SHANGHAI, 2024, 41(6): 46
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Received: Jan. 26, 2024
Accepted: --
Published Online: Mar. 7, 2025
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