Impact modeling for the Double Asteroid Redirection Test (DART) mission
Introduction
The Asteroid Impact Deflection Assessment (AIDA) collaboration is a joint ESA-NASA planetary defense collaboration that will include the first full-scale test of an asteroid deflection by kinetic impactor [1]. The AIDA collaboration comprises two independent spacecraft, the NASA-sponsored Double Asteroid Redirection Test (DART) and the ESA-led Hera. In September 2022 the DART spacecraft will impact the secondary member of the binary asteroid system 65,803 Didymos (Didymos-B) at a speed of ~6.7 km/s and mass ~500 kg (Fig. 1). The resulting period change in the orbit of Didymos-B will be measured using Earth-based observations. Hera will arrive post-impact and perform detailed measurements to characterize Didymos-B.
Post-impact, the measured period change of Didymos-B will be used to compute the momentum transferred to the asteroid by the DART spacecraft. It is expected that the momentum change induced by DART could be larger than the incoming spacecraft momentum due to ejecta escaping from Didymos-B. This momentum enhancement effect is well-known and has been studied using both models and experiments [e.g., [2], [3], [4]] and is commonly parameterized by a momentum enhancement factor β, whereand ptarget is the momentum change of the target post-impact, pimpactor is the initial momentum of the impactor, and pejecta is the momentum carried by escaping ejecta. The properties of Didymos-B are poorly known and the local conditions of the specific impact site on the body influence the impact event; these factors result in high uncertainty in the expected momentum transfer of the DART impact. Early modeling efforts have found that β could reasonably be as low as ~1 or greater than 5 in end-member cases [5,6].
Studies of kinetic impactors have shown that the momentum enhancement factor β varies significantly with impact velocity, impact geometry, target internal structure and material properties [e.g., 7,8]. In order to apply the results of the DART impact to the design of future kinetic deflection missions, the relationship between β and asteroid properties must be well-understood.
Numerical simulations will be the primary tool used for interpretation of the measured period change of Didymos-B in terms of the momentum enhancement factor β resulting from the DART impact and its broader implications for kinetic deflection of asteroids. The Impact Simulation Working Group, which is part of the DART Investigation Team, is tasked with using impact modeling both pre- and post-impact to estimate the range of impact outcomes, including β, crater morphology, and ejecta properties, to calculate the relationships between the measured deflection and the asteroid physical properties, and to infer properties of Didymos-B based on post-impact measurements. Initial studies by the Impact Simulation Working Group have also included a benchmarking campaign [9] to characterize the variability in results from different numerical impact models used by the community, which showed that when using similar material properties the impact models produced similar results for crater size and momentum transfer. Previous studies have shown that numerical impact models can reproduce crater sizes, ejecta masses, and momentum transfer measured in laboratory experiments [e.g., 10,11]; however, application of these models for momentum transfer in planetary impacts at orders of magnitude larger scale cannot be easily tested. The DART impact will provide rare and valuable planetary-scale validation data for these numerical impact models, increasing confidence in the use of numerical models for design of kinetic impactor missions.
Because the physical properties of Didymos-B are poorly known, using numerical models to interpret the DART impact outcome will require running simulations over a wide range of potential material properties and internal structures. In this paper we present results from a sensitivity study of the effect of bulk material properties on the DART impact outcome using homogeneous asteroid target models. This purposes of this study are (1) to determine a range of potential outcomes for the DART impact, (2) to determine which model inputs are significant predictors of the DART impact outcome, and (3) to reduce the parameter space required for future, more complex simulations.
Like other asteroids [e.g., 12], Didymos-B may be a “rubble pile” agglomeration of rocks with sizes ranging from pebbles to boulders along with loosely consolidated sediments, rather than a relatively homogeneous rocky object. Due to computing limitations, it is not possible to separately model individual grains or pebbles within a full-scale planetary impact simulation (though large boulders can be individually modeled). Agglomerations of smaller particles are typically modelled as a continuous matrix with an average porosity and bulk strength properties. Simulations of impacts with rubble pile asteroids have shown that the impact outcome is highly dependent on the local impact site materials: whether the kinetic impactor hits sediment or competent rock has a significant influence on the total momentum transferred to the asteroid [8]. In the future, results of this study can be used to relate continuum approximations of rubble pile models to bulk properties, and also to facilitate comparisons of DART impact simulations performed with different impact modeling codes. Different codes contain different implementations of common asteroid material models, and not all model inputs have a one-to-one correspondence; therefore, knowledge of which model inputs are significant for DART momentum transfer will greatly simplify these types of comparisons.
Section snippets
Material property sensitivity study
For this study, a set of 2D axisymmetric simulations was run using CTH, a shock physics Eulerian hydrocode developed by Sandia National Laboratories [13]. The use of 2D models allows for a large number of fast-running simulations at high resolution, but does not allow for variable impact geometries (only vertical impacts were modelled) or the complex shape of the DART spacecraft. 3D simulations will be used in the future to explore these effects.
Results
The calculated β and crater width/depth ratios for all CTH runs were analyzed using JMP to determine which inputs had highest statistical significance for predicting the CTH simulation results. The results showed that β is influenced by a relatively small number of target strength parameters, while crater morphology is influenced by the same target strength parameters as well as impactor shape. The parameters with highest statistical significance for predicting β were target porosity, yield
Conclusions
The results of this study show that for realistic combinations of asteroid material properties, the DART impact would be expected to produce a β between 1.5 and 2. In addition, the outcome of the DART impact is expected to be primarily driven by a relatively small number of material properties, in particular strength and porosity. Note that the number of significant inputs found here is smaller than in the sensitivity study carried out by Bruck Syal et al. [7], who considered a much broader
Acknowledgments
This study was funded by NASA for the Double Asteroid Redirection Test (DART) Phase C-D, contract NNN06AA01C to Johns Hopkins University Applied Physics Laboratory.
References (26)
- et al.
AIDA DART asteroid deflection test: planetary defense and science objectives
Planet Space Sci
(2018) - et al.
Momentum enhancement in hypervelocity impact
Int J Impact Eng
(2011) - et al.
Momentum transfer in asteroid impacts I. Theory and scaling
Icarus
(2012) - et al.
Modeling momentum transfer from kinetic impacts: implications for redirecting asteroids
Procedia Eng
(2015) - et al.
Modeling impact outcomes for the Double Asteroid Redirection Test (DART) mission
Procedia Eng
(2017) - et al.
Hypervelocity impact on pumice: scale effects on experiments and simulations
Procedia Eng
(2017) - et al.
Size scaling of hypervelocity-impact ejecta mass and momentum enhancement: experiments and a nonlocal-shear-band-motivated strain-rate-dependent failure model
Int J Impact Eng
(2020) - et al.
CTH: a three-dimensional shock wave physics code
Int J Impact Eng
(1990) Theoretical equation of state for aluminum
Int J Impact Eng
(1987)- et al.
Dynamic fault weakening and the formation of large impact craters
Earth Planet. Sci. Lett.
(2009)
Numerical simulations of impacts involving porous bodies I: implementing sub-resolution porosity in a 3-D SPH hydrocode
Icarus
Hypervelocity impacts on asteroids and momentum transfer I. Numerical simulations using porous targets
Icarus
Deflection by kinetic impact: sensitivity to asteroid properties
Icarus
Cited by (24)
Effectiveness analysis of multiple kinetic impacts of near-Earth asteroids
2022, Advances in Space ResearchThe Secular Dynamical Evolution of Binary Asteroid System (65803) Didymos Post-DART
2024, Planetary Science JournalAchievement of the Planetary Defense Investigations of the Double Asteroid Redirection Test (DART) Mission
2024, Planetary Science Journal