Planetary defense

LLNL scientists use large-scale simulations on supercomputers to evaluate different methods for defending the planet from asteroid collisions.

Addressing a potential threat

Our planet has been continually bombarded by asteroids since its formation. While the frequency of large impacts has decreased, many potential Near-Earth Object (NEO) threats remain undiscovered, so if or when they will impact Earth remains unknown.

Most of the time, an impacting asteroid will simply burn up in the atmosphere, resulting in a meteor shower display. However, Earth-bound objects only a few kilometers across have already caused global catastrophes, such as the impact that wiped out all non-avian dinosaurs and many other species 66 million years ago and the more recent Chelyabinsk meteor, which injured hundreds of people and damaged many structures.

Our team of physicists, material scientists, geoscientists, engineers, and computational physicists are working with collaborators across several national labs, universities, and international research centers to develop methods for detecting and mitigating the next large Earth-bound object. Leveraging LLNL’s high-performance computing and high-energy-density capabilities, we characterize NEOs, simulate methods to nudge the trajectory of those that pose a threat, and model impact consequences to inform emergency response.

Three planetary defense team members.
Mike Owen, Katie Kumamoto, and Megan Bruck Syal at the DART mission impact event at the Johns Hopkins University Applied Physics Laboratory.

Disruption and deflection with nuclear explosives

Simulation results compare well with the actual impact.
Our team uses Spheral, an Adaptive Smoothed Particle Hydrodynamics (ASPH) code, to model high-speed impact events, including the mega-crater Stickney, which dominates the shape of Phobos, a Martian moon (left). Previous modeling of the impact event was unable to replicate Stickney without globally fragmenting the satellite. High-resolution numerical simulations, using Spheral, successfully generated Stickney crater while maintaining the large-scale structure of Phobos. Target porosity, which is estimated to be significant, aids in keeping the moon intact.

For scenarios with little warning time before impact or when the object is large, the most effective approach is using a nuclear explosive to either disrupt or deflect the asteroid. Our team has developed the modeling capability to evaluate nuclear approaches that can be used to deflect (gently nudge) or disrupt (break up, disperse the fragments) an incoming asteroid.

Because asteroids and comets vary in size, density, composition, dynamics, and internal structure, we consider cases that span observed behavior and properties. We use different simulation capabilities, uncertainty quantification techniques, radiation hydrodynamics codes, and advanced algorithms to examine the physical processes involved in a nuclear detonation, the subsequent energy production and deposition, the material’s response, and debris dispersal after the disruption.

Our simulations of deflection by means of nuclear explosion have yielded valuable understanding of scenarios in which a large asteroid bears down on Earth with little warning. Additional research includes predictive modeling using energy and density inputs based on actual NEOs observed in the solar system. By better understanding the available threat-mitigation options and their outcomes, our models will help improve confidence in the effectiveness of a nuclear response should the need arise.

Characterizing asteroid material

Without convenient, cost-effective ways to experiment directly on asteroids in the solar system, we use high-energy-density experiments on asteroid fragments to validate and improve our models. These experiments leverage the high-power laser capabilities at LLNL’s Jupiter Laser Facility to study the samples under extreme conditions.

In one such study, we collaborated with the University of Oxford to conduct experiments on rare meteoritic samples using Janus, a kilojoule-class, neodymium-glass laser system. The results allowed us to gauge each sample’s strength and work on the material’s equation of state.

Validation with impact

Building on our previous simulation efforts, we have also modeled a nonnuclear deflection method known as kinetic impact. This method involves ramming an impactor—an uncrewed spacecraft—against an asteroid at high speeds, typically many kilometers per second (tens of thousands of miles per hour). The impact delivers the momentum of the spacecraft, plus additional momentum from cratering ejecta thrown off the asteroid’s surface. This momentum delivery slightly changes the asteroid’s velocity; if the velocity is changed with enough warning time, it can cause a potential Earth-impactor to miss the Earth. Even within the limited parameters for this method to work, the variables associated with the kinetic impact method are numerous. The research requires experts from many fields working together to build models incorporating realistic asteroid properties and to run simulations on large computer clusters.

This work led to our collaboration with NASA and the Johns Hopkins Applied Physics Laboratory to support NASA’s Double Asteroid Redirection Test (DART) mission, the first demonstration of the kinetic impactor technique to change the motion of an asteroid in space. DART targeted Dimorphos, a small moonlet (150-meter diameter) orbiting a larger asteroid, named Didymos (800-meter diameter). Targeting a binary asteroid allowed a precise measurement of the velocity change imparted by DART by measuring the orbital period before and after the impact, using Earth-based telescopes. In preparation for DART, our team investigated various impact scenarios and developed new methods to simulate the range of possible asteroid targets and to model the DART spacecraft with higher fidelity. The LLNL-developed Spheral code was used to carry out all the impact simulations provided by LLNL in support of the DART mission.

Simulations showing ejecta from two DART-like impacts.
Pre-impact simulations for the DART mission used a scaled-down shape model of the asteroid Itokawa as part of an inverse test to practice the handoff of information from proximity operations to impact modelers, who then must simulate the range of initial conditions that are consistent with measurements from the impact experiment. Remarkably, both simulations impart a similar delta-v to the asteroid; the left is more porous (lighter) and stronger, while the right is less porous (heavier) and weaker. This work is part of an expansive 3D study led by LLNL’s Kathryn Kumamoto.

Shortly after the DART impact experiment, NASA announced that the spacecraft successfully changed the asteroid’s motion in space, shortening the orbital period from 11 hours and 55 minutes to 11 hours and 23 minutes. Our researchers are using this period change measurement, combined with the final images of Dimorphos from the DART spacecraft and other data from Earth- and space-based telescopes, to determine what target properties are consistent with the asteroid’s change in velocity. Using DART’s final pre-impact images, the team will also build a realistic target shape and structure while implementing high-fidelity models of the DART spacecraft’s geometry.

Making the world safer

Our planetary defense program grew out of the capabilities and expertise developed and refined in LLNL’s weapons program. LLNL is one of a few places worldwide with the simulation capability and the knowledge of nuclear-explosives effects to conduct this research. By applying our expertise to extraterrestrial threats, we continue to support and expand the Laboratory’s mission to make the world a safer place.

Other teams at LLNL contribute to planetary defense by pursuing hazardous asteroid discovery and orbit characterization using astronomical surveys and advanced data science techniques. For more information, see the Optical astronomy and cosmology research page.


Name Title Discipline


Johns Hopkins University Applied Physics Laboratory (JHUAPL)

NASA Goddard Space Flight Center (GSFC)

NASA Ames Research Center (ARC)

NASA Jet Propulsion Laboratory (JPL)

NASA Marshall Space Flight Center (MSFC)

NASA Johnson Space Center (JSC)

Los Alamos National Laboratory (LANL)

Sandia National Laboratory (SNL)

University of Colorado Boulder

University of Maryland, College Park

Observatoire de la Côte d'Azur (Nice Observatory)

Select publications