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NEOSHIELD - A Global Approach to Near-earth Object Impact Threat Mitigation

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Handbook of Cosmic Hazards and Planetary Defense

Abstract

NEOShield, a project funded by the European Commission, brings together an international team of 13 partner organizations to address the global issue of near-Earth objects (NEO) impact prevention. The project’s goals are to investigate the feasibility of techniques to prevent a potentially catastrophic impact on Earth by an asteroid or a comet and to develop detailed designs of appropriate missions to test deflection techniques.

This chapter highlights some of the NEOShield research results obtained to date. The focus will be on mitigation-related science with a brief discussion of ongoing technology development and test-mission designs. Following a brief introduction to the NEOShield project, the three main NEO deflection techniques investigated are described (the kinetic impactor, blast deflection, and the gravity tractor), and the required or desirable payload instrumentation for each technique is discussed. A necessary prerequisite for the design of a successful deflection mission is accurate knowledge of the relevant physical properties of the threatening object; therefore, some of the key physical properties are addressed. A crucial component of NEOShield is laboratory and numerical modeling work to complement investigations of NEO physical properties based on observational data. Experiments to measure the momentum transfer during hypervelocity impacts into different asteroid analog materials are described, as well as initial results of numerical simulations of kinetic impacts at various velocities into small asteroids with different porosities.

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References

  • Benz W, Asphaug E (1995) Simulations of brittle solids using smooth particle hydrodynamics. Comput Phys Commun 87:253–265

    Article  MATH  Google Scholar 

  • Chesley SR, Spahr TB (2004) Earth impactors: orbital characteristics and warning times. In: Belton M, Morgan TH, Samarasinha N, Yeomans DK (eds) Mitigation of hazardous comets and asteroids. Cambridge University Press, Cambridge, pp 22–37

    Chapter  Google Scholar 

  • DeMeo EF, Binzel RP, Slivan SM, Bus SJ (2009) An extension of the bus asteroid taxonomy into the near-infrared. Icarus 202:160–180

    Article  Google Scholar 

  • Farnocchia D, Bernardi F, Valsecchi GB (2012) Efficiency of a wide-area survey in achieving short- and long-term warning for small impactors. Icarus 219(1):41–47

    Article  Google Scholar 

  • Harris AW, Drube L (2014) How to find metal-rich asteroids. Astrophys J Lett 785:L4. doi:10.1088/2041-8205/785/1/L4

    Article  Google Scholar 

  • Harris AW, Barucci MA, Cano JL, Fitzsimmons A, Fulchignoni M, Green SF, Hestroffer D, Lappas V, Lork W, Michel P, Morrison D, Payson D, Schäfer F (2013) The European Union funded NEOShield project: a global approach to near-Earth object impact threat mitigation. Acta Astronautica 90(1):80–84. doi:10.1016/j.actaastro.2012.08.026

    Google Scholar 

  • Holsapple KA, Housen KR (2012) Momentum transfer in asteroid impacts. Theory and scaling. Icarus 221:875–887

    Article  Google Scholar 

  • Housen KR, Holsapple KA (2011) Ejecta from impact craters. Icarus 211:856–875

    Article  Google Scholar 

  • Housen KR, Holsapple KA (2012) Deflecting asteroids by impacts: what is beta? 43rd LPSC, LPI Contribution No 1659

    Google Scholar 

  • Jutzi M, Michel P (2014) Hypervelocity impacts on asteroids and momentum transfer I. Numerical simulations using porous targets. Icarus 229:247–253

    Article  Google Scholar 

  • Jutzi M, Benz W, Michel P (2008) Numerical simulations of impacts involving porous bodies. I. Implementing sub-resolution porosity in a 3D SPH hydrocode. Icarus 198:242–255

    Article  Google Scholar 

  • Jutzi M, Asphaug E, Gillet P, Barrat J-A, Benz W (2013) The structure of the asteroid 4 Vesta as revealed by models of planet-scale collisions. Nature 494:207–210

    Article  Google Scholar 

  • Lu ET, Love SG (2005) Gravitational tractor for towing asteroids. Nature 438:177–178

    Article  Google Scholar 

  • Mainzer A et al (2011) NEOWISE observations of near-Earth objects: preliminary results. Astrophys J 743(156):17

    Google Scholar 

  • Rathke A, Izzo D (2007) Keplerian consequences of an impact on an asteroid and their relevance for a deflection demonstration mission. In: Valsecchi GB, Vokrouhlický D, Milani A (eds) Near Earth objects, our celestial neighbors: opportunity and risk. Proceedings of IAU symposium 236. Cambridge University Press, Cambridge, pp 417–426

    Google Scholar 

  • Sánchez P, Scheeres DJ (2013) The strength of regolith and rubble pile asteroids. arXiv:1306.1622v1 [astro-ph.EP]

    Google Scholar 

  • Tholen DJ (1984) Asteroid taxonomy from cluster analysis of photometry. PhD thesis, University of Arizona

    Google Scholar 

  • Tonry JL (2011) An early warning system for asteroid impact. Publ Astron Soc Pac 123(899):58–73

    Article  Google Scholar 

Download references

Acknowledgments

The porosity of the target materials for the hypervelocity impact experiments was determined at Albert-Ludwigs-Universität Freiburg by Dr. Müller-Siegmund. The laboratory experiments could not have been made without the valuable assistance of the EMI technicians running the light-gas accelerator and the interns Dominik Haas, Georg Schäfer, Nico Reichenbach, Philipp Rotter, Daniela Weimer, and David Muessle for their valuable assistance in conducting the impact experiments and analyzing the results.

This publication makes use of data products from NEOWISE, which is a project of the Jet Propulsion Laboratory/California Institute of Technology, funded by the Planetary Science Division of the National Aeronautics and Space Administration.

The research leading to these results has received funding from the European Union’s Seventh Framework Programme (FP7/2007–2013) under grant agreement n° 282703 (NEOShield).

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Correspondence to L. Drube .

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Drube, L., Harris, A.W., Hoerth, T., Michel, P., Perna, D., Schäfer, F. (2015). NEOSHIELD - A Global Approach to Near-earth Object Impact Threat Mitigation. In: Pelton, J., Allahdadi, F. (eds) Handbook of Cosmic Hazards and Planetary Defense. Springer, Cham. https://doi.org/10.1007/978-3-319-03952-7_61

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