Enhanced kinetic impactor for deflecting large potentially hazardous asteroids via maneuvering space rocks
Li, Mingtao and Wang, Yirui and Wang, Youliang and Zhou, Binghong and Zheng, Wei (2020) Enhanced kinetic impactor for deflecting large potentially hazardous asteroids via maneuvering space rocks. Scientific Reports, 10. 8506. ISSN 2045-2322 (https://doi.org/10.1038/s41598-020-65343-z)
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Abstract
Asteroid impacts pose a major threat to all life on Earth. The age of the dinosaurs was abruptly ended by a 10-km-diameter asteroid. Currently, a nuclear device is the only means of deflecting large Potentially Hazardous Asteroids (PHAs) away from an Earth-impacting trajectory. The Enhanced Kinetic Impactor (EKI) concept is proposed to deflect large PHAs via maneuvering space rocks. First, an unmanned spacecraft is launched to rendezvous with an intermediate Near-Earth Asteroid (NEA). Then, more than one hundred tons of rocks are collected from the NEA as the EKI. The NEA can also be captured as the EKI if the NEA is very small. Finally, the EKI is maneuvered to impact the PHA at a high speed, resulting in a significant deflection of the PHA. For example, to deflect Apophis, as much as 200 t of rocks could be collected from a NEA as the EKI based on existing engineering capabilities. The EKI can produce a velocity increment (∆v) of 39.81 mm/s in Apophis, thereby increasing the minimum geocentric distance during the close encounter in 2029 by 1,866.93 km. This mission can be completed in 3.96 years with a propellant cost of 2.98 t. Compared with a classic kinetic impactor, the deflection distance can be increased one order of magnitude. The EKI concept breaks through the limitation of the ground-based launch capability, which can significantly increase the mass of the impactor. We anticipate that our research will be a starting point for efficient planetary defense against large PHAs.
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Item type: Article ID code: 95107 Dates: DateEvent22 May 2020PublishedSubjects: Science > Astronomy Department: Faculty of Engineering > Mechanical and Aerospace Engineering Depositing user: Pure Administrator Date deposited: 05 Jan 2026 10:24 Last modified: 22 Jan 2026 09:42 URI: https://strathprints.strath.ac.uk/id/eprint/95107
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