On the consequences of a fragmentation due to a NEO mitigation strategy

The fragmentation of an Earth threatening asteroid as a result of a hazard mitigation mission is examined in this paper. The minimum required energy for a successful impulsive deflection of a threatening object is computed and compared with the energy required to break-up a small size asteroid. The fragmentation of an asteroid that underwent an impulsive deflection such as a kinetic impact or a nuclear explosion is a very plausible outcome in the light of this work. Thus a model describing the stochastic evolution of the cloud of fragments is described. The stochasticity of the fragmentation is given by a Gaussian probability distribution that describes the initial relative velocities of each fragment of the asteroid, while the size distribution is expressed through a power law function. The fragmentation model is applied to Apophis as illustrative example. If a barely catastrophic disruption (i.e. the largest fragment is half the size of the original asteroid) occurs 10 to 20 years prior to the Earth encounter only a reduction from 50% to 80% of the potential damage is achieved for the Apophis test case.

[1]  R. P. Young,et al.  Experimental hypervelocity impact effects on simulated planetesimal materials , 1994 .

[2]  John L. Remo Energy requirements and payload masses for near-Earth objects hazard mitigation , 2000 .

[3]  Matthew A. Vavrina,et al.  1st ACT global trajectory optimisation competition: Results found at the Jet Propulsion Laboratory , 2007 .

[4]  Eileen V. Ryan,et al.  On collisional disruption - Experimental results and scaling laws , 1990 .

[5]  William K. Hartmann,et al.  Planetesimals to planets: Numerical simulation of collisional evolution , 1978 .

[6]  Keith A. Holsapple,et al.  Catastrophic disruptions and cratering of solar system bodies: a review and new results , 1994 .

[7]  H. Melosh,et al.  NON-NUCLEAR STRATEGIES FOR DEFLECTING COMETS AND ASTEROIDS , 2021, Hazards Due to Comets and Asteroids.

[8]  H. J. Moore,et al.  Spray Ejected from the Lunar Surface by Meteoroid Impact , 1963 .

[9]  R. Greenberg,et al.  Steady-State Size Distributions for Collisional Populations: Analytical Solution with Size-Dependent Strength , 2003, 1407.3307.

[10]  Alan W. Harris,et al.  The Rotation Rates of Very Small Asteroids: Evidence for Rubble-Pile Structure , 1996 .

[11]  L. W. Alvarez,et al.  Extraterrestrial Cause for the Cretaceous-Tertiary Extinction , 1980, Science.

[12]  G. Radice,et al.  Multi-criteria Comparison among Several Mitigation Strategies for Dangerous Near Earth Objects , 2010 .

[13]  Steven R. Chesley,et al.  Mitigation of Hazardous Comets and Asteroids: Earth impactors: orbital characteristics and warning times , 2004 .

[14]  Colin R. McInnes,et al.  Deflection of near-Earth asteroids by kinetic energy impacts from retrograde orbits , 2004 .

[15]  H. J. Melosh,et al.  Impact Fragmentation: From the Laboratory to Asteroids☆ , 1998 .

[16]  V. V. Ivashkin,et al.  An analysis of some methods of asteroid hazard mitigation for the Earth , 1995 .

[17]  M. P. Goda,et al.  The fragmentation of small asteroids in the atmosphere , 1993 .

[18]  T. Ahrens,et al.  Deflection and fragmentation of near-Earth asteroids , 1992, Nature.

[19]  Steven R. Chesley,et al.  A Quantitative Assessment of the Human and Economic Hazard from Impact-generated Tsunami , 2006 .

[20]  David Morrison,et al.  Impacts on the Earth by asteroids and comets: assessing the hazard , 1994, Nature.

[21]  W. Wiesel Fragmentation of asteroids and artificial satellites in orbit , 1978 .

[22]  Y. Takagi,et al.  New scaling laws on impact fragmentation , 1990 .

[23]  Gianmarco Radice,et al.  Multicriteria Comparison Among Several Mitigation Strategies for Dangerous Near-Earth Objects , 2009 .

[24]  K. Holsapple THE SCALING OF IMPACT PROCESSES IN PLANETARY SCIENCES , 1993 .