Kinetic deflection change due to target global curvature as revealed by NASA/DART

dc.contributor.authorHirabayashi, Masatoshi
dc.contributor.authorRaducan, Sabina D.
dc.contributor.authorSunshine, Jessica M.
dc.contributor.authorFarnham, Tony L.
dc.contributor.authorLolachi, Ramin
dc.contributor.authoret al
dc.date.accessioned2024-02-06T18:02:19Z
dc.date.available2024-02-06T18:02:19Z
dc.date.issued2024-01-16
dc.descriptionAuthors: Masatoshi Hirabayashi, Sabina D. Raducan, Jessica M. Sunshine, Tony L. Farnham, J. D. Prasanna Deshapriya, Jian-Yang Li, Gonzalo Tancredi, Steven R. Chesley, R. Terik Daly, Carolyn M. Ernst, Igor Gai, Pedro H. Hasselmann, Shantanu P. Naidu, Hari Nair, Eric E. Palmer, C. Dany Waller, Angelo Zinzi, Harrison F. Agrusa, Brent W. Barbee, Megan Bruck Syal, Gareth S. Collins, Thomas M. Davison, Mallory E. DeCoster, Martin Jutzi, Kathryn M. Kumamoto, Nicholas A. Moskovitz, Joshua R. Lyzhoft, Stephen R. Schwartz, Paul A.
dc.description.abstractKinetic deflection is a planetary defense technique that delivers spacecraft momentum to a small body to deviate its course from Earth. The deflection efficiency depends strongly on the impactor and target. Among them, the contribution of global curvature was poorly understood. The ejecta plume created by NASA's DART impact on its target asteroid, Dimorphos, exhibited an elliptical shape almost aligned along its north-south direction. Here, we identify that this elliptical ejecta plume resulted from the target’s curvature, reducing the momentum transfer to 44±10% along the orbit track compared to an equivalent impact on a flat target. We also find lower kinetic deflection of impacts on smaller Near-Earth objects (NEOs) due to higher curvature. A solution to mitigate low deflection efficiency is to apply multiple low-energy impactors rather than a single high-energy impactor. Rapid reconnaissance to acquire a target's properties before deflection enables determining the proper locations and timing of impacts.
dc.description.sponsorshipThis work was supported by the DART mission, NASA Contract No. 80MSFC20D0004. This work was supported by the Italian Space Agency (ASI) within the LICIACube project (ASI-INAF agreement n. 2019-31-HH.0 and its extension 2019-31-HH.1-2022). This work is partially supported by NASA through grant HSTGO-16674 from the Space Telescope Science Institute, which is operated by the Association of Universities for Research in Astronomy, Inc., under NASA contract NAS 5-26555. Portions of this work were performed by Lawrence Livermore National Laboratory under DOE contract DE-AC52-07NA27344. LLNL-JRNL-853920. S.D.R. and M.J. acknowledge support from the Swiss National Science Foundation (project number 200021 207359). Work of E.G.F., S.P.N., and S.R.C. was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration (80NM0018D0004). R.M. acknowledges funding from a NASA Space Technology Graduate Research Opportunities (NSTGRO) award, NASA contract No. 80NSSC22K1173. P.M. acknowledges funding support from the French Space Agency CNES and The University of Tokyo. G.T. acknowledges financial support from project FCE-1-2019-1-156451 of the Agencia Nacional de Investigación e Innovación ANII and Grupos I+D 2022 CSIC-Udelar (Uruguay). The work by J.O. was supported by grant PID2021-125883NB-C22 by the Spanish Ministry of Science and Innovation/State Agency of Research MCIN/AEI/ 10.13039/501100011033 and by “ERDF A way of making Europe." The work by J.O. and I.H. was supported by the Spanish Research Council (CSIC) support for international cooperation: I-LINK project ILINK22061. S.R.S. acknowledges support from the DART Participating Scientist Program, grant no. 80NSSC22K0318. This research was supported in part through research cyberinfrastructure resources and services provided by the Partnership for an Advanced Computing Environment (PACE) at the Georgia Institute of Technology. The authors also acknowledge Mark Cintala for detailed reviews and proofreading of this manuscript.
dc.description.urihttps://www.researchsquare.com/article/rs-3598104/v1
dc.format.extent27 pages
dc.genrejournal articles
dc.genrepreprints
dc.identifier.urihttps://doi.org/10.21203/rs.3.rs-3598104/v1
dc.identifier.urihttp://hdl.handle.net/11603/31565
dc.language.isoen_US
dc.relation.isAvailableAtThe University of Maryland, Baltimore County (UMBC)
dc.relation.ispartofUMBC Center for Space Sciences and Technology
dc.relation.ispartofUMBC Faculty Collection
dc.rightsThis work was written as part of one of the author's official duties as an Employee of the United States Government and is therefore a work of the United States Government. In accordance with 17 U.S.C. 105, no copyright protection is available for such works under U.S. Law.
dc.rightsPDM 1.0 DEED Public Domain Mark 1.0 Universalen
dc.rights.urihttps://creativecommons.org/publicdomain/mark/1.0/
dc.titleKinetic deflection change due to target global curvature as revealed by NASA/DART
dc.typeText
dcterms.creatorhttps://orcid.org/0000-0001-5764-7639

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