Abstract
The Chicxulub asteroid impact triggered mass extinction, mega-tsunamis and a spell of global warming that lasted for around 100,000 years. Although the recent Double Asteroid Redirection Test mission by NASA demonstrated that near-Earth objects can be successfully targeted, deflecting the most dangerous asteroids will require energy concentrations akin to nuclear explosions. However, targets suitable for practice missions are scarce. Here we demonstrate the simulation of asteroid deflection with an X-ray pulse from a dense argon plasma generated at the Z machine, a pulsed power device at Sandia National Laboratories. We use so-called X-ray scissors to place surrogate asteroidal material into free space, simultaneously severing supports and vapourizing the target surface. The ensuing explosion accelerates the mock asteroidal material in a scaled asteroid intercept mission. Deflection velocities of around 70 m s–1 for silica targets agree with radiation-hydrodynamic model predictions. We scale these results to proposed interceptor energies and predict that asteroids up to a diameter of (4 ± 1) km can be deflected with this mechanism, showing a viable way to prepare for future planetary defence missions.
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Acknowledgements
We thank M. Abere, P. Codding, A. Harvey-Thompson, D. Johnson, C. Kunka, D. Lamppa, J. Marks, V. Martinez, A. McCourt, R. Obregon, L. Pacheco, S. Payne, R. Schecker, D. Thompson and K. Vigil for experimental support, K. Amodeo, J. Carpenter, D. Dolan, T. Mattsson, J. Niederhaus and S. Payne for useful discussions and the Z machine operations and diagnostic teams. Sandia National Laboratories is a multi-mission laboratory managed and operated by National Technology & Engineering Solutions of Sandia, LLC (NTESS), a wholly owned subsidiary of Honeywell International Inc., for the US Department of Energy (DOE) National Nuclear Security Administration (DOE/NNSA) under contract no. DE-NA0003525. This written work is authored by an employee of NTESS. The employee, not NTESS, owns the right, title and interest in and to the written work and is responsible for its contents. Any subjective views or opinions that might be expressed in the written work do not necessarily represent the views of the US Government. The publisher acknowledges that the US Government retains a non-exclusive, paid-up, irrevocable, worldwide license to publish or reproduce the published form of this written work or allow others to do so, for US Government purposes. The DOE will provide public access to results of federally sponsored research in accordance with the DOE Public Access Plan.
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N.W.M. and S.R. conceived the experiment. N.W.M., J.J.S. and C.R.A. designed and developed the experimental apparatus. C.A.M. built the apparatus. N.W.M. and M.-A.S. designed the experiments. M.-A.S. and C.A.M. carried out the experiments. N.W.M. and M.-A.S. processed the data. N.W.M. developed the analytical model. M.M., J.J.S., N.W.M., M.J.P. and K.R.C. developed the finite element models and performed the analysis. N.W.M. and M.M. interpreted the data. N.W.M. and M.-A.S. wrote the paper. All authors contributed to reviewing the manuscript.
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Extended data
Extended Data Fig. 1 X-ray spectrum of argon gas puff source.
The main panel shows the measured x-ray spectrum (black) and ±1-σ uncertainty bounds (shaded). The inset shows the spectrum after numerical propagation through the beryllium x-ray filter used in the experiment, that is, incident onto the silica targets, on a linear scale, showing that the spectrum reaching the target predominantly consists of K-shell line emission from the argon plasma.
Extended Data Fig. 2 Geometry of asteroid deflection scenario.
The figure illustrates the distances and angles used in the derivation of Eq. 7, including cartesian coordinates for the x-ray source at the interceptor position \(\left\{{x}_{0},0\right\},\) maximum tangent intercept \(\left\{x{\prime} ,y{\prime} \right\}\), and local tangent intercept \(\left\{{x}_{I},{y}_{I}\right\}\) at distance \(d\), for an asteroid target with radius \(r\) and stand-off distance \(\Lambda\), and indicated subtended angles. Arrow at right indicates the direction of the target velocity change \(\Delta v\) from the nuclear intercept.
Source data
Source Data Fig. 2
Data for Fig. 2.
Source Data Fig. 4
Data for Fig. 4.
Source Data Extended Data Fig. 1
Data for Extended Data Fig. 1.
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Moore, N.W., Mesh, M., Sanchez, J.J. et al. Simulation of asteroid deflection with a megajoule-class X-ray pulse. Nat. Phys. (2024). https://doi.org/10.1038/s41567-024-02633-7
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DOI: https://doi.org/10.1038/s41567-024-02633-7