Predictions for the Dynamical States of the Didymos System before and after the Planned DART Impact

Author:

Richardson Derek C.ORCID,Agrusa Harrison F.ORCID,Barbee Brent,Bottke William F.ORCID,Cheng Andrew F.ORCID,Eggl SiegfriedORCID,Ferrari FabioORCID,Hirabayashi MasatoshiORCID,Karatekin Özgür,McMahon JayORCID,Schwartz Stephen R.ORCID,Ballouz Ronald-LouisORCID,Bagatin Adriano CampoORCID,Dotto ElisabettaORCID,Fahnestock Eugene G.,Fuentes-Muñoz OscarORCID,Gkolias Ioannis,Hamilton Douglas P.,Jacobson Seth A.ORCID,Jutzi MartinORCID,Lyzhoft Josh,Makadia RahilORCID,Meyer Alex J.ORCID,Michel PatrickORCID,Nakano RyotaORCID,Noiset GuillaumeORCID,Raducan Sabina D.ORCID,Rambaux Nicolas,Rossi AlessandroORCID,Sánchez PaulORCID,Scheeres Daniel J.ORCID,Soldini StefaniaORCID,Stickle Angela M.ORCID,Tanga PaoloORCID,Tsiganis KleomenisORCID,Zhang YunORCID

Abstract

Abstract NASA’s Double Asteroid Redirection Test (DART) spacecraft is planned to impact the natural satellite of (65803) Didymos, Dimorphos, at around 23:14 UTC on 2022 September 26, causing a reduction in its orbital period that will be measurable with ground-based observations. This test of kinetic impactor technology will provide the first estimate of the momentum transfer enhancement factor β at a realistic scale, wherein the ejecta from the impact provide an additional deflection to the target. Earth-based observations, the LICIACube spacecraft (to be detached from DART prior to impact), and ESA’s follow-up Hera mission, to launch in 2024, will provide additional characterizations of the deflection test. Together, Hera and DART comprise the Asteroid Impact and Deflection Assessment cooperation between NASA and ESA. Here, the predicted dynamical states of the binary system upon arrival and after impact are presented. The assumed dynamically relaxed state of the system will be excited by the impact, leading to an increase in eccentricity and a slight tilt of the orbit, together with enhanced libration of Dimorphos, with the amplitude dependent on the currently poorly known target shape. Free rotation around the moon’s long axis may also be triggered, and the orbital period will experience variations from seconds to minutes over timescales of days to months. Shape change of either body, due to cratering or mass wasting triggered by crater formation and ejecta, may affect β, but can be constrained through additional measurements. Both BYORP and gravity tides may cause measurable orbital changes on the timescale of Hera’s rendezvous.

Funder

National Aeronautics and Space Administration

Publisher

American Astronomical Society

Subject

Space and Planetary Science,Earth and Planetary Sciences (miscellaneous),Geophysics,Astronomy and Astrophysics

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