Abstract
Most near-Earth objects came from the asteroid belt and drifted via non-gravitational thermal forces into resonant escape routes that, in turn, pushed them onto planet-crossing orbits1,2,3. Models predict that numerous asteroids should be found on orbits that closely approach the Sun, but few have been seen. In addition, even though the near-Earth-object population in general is an even mix of low-albedo (less than ten per cent of incident radiation is reflected) and high-albedo (more than ten per cent of incident radiation is reflected) asteroids, the characterized asteroids near the Sun typically have high albedos4. Here we report a quantitative comparison of actual asteroid detections and a near-Earth-object model (which accounts for observational selection effects). We conclude that the deficit of low-albedo objects near the Sun arises from the super-catastrophic breakup (that is, almost complete disintegration) of a substantial fraction of asteroids when they achieve perihelion distances of a few tens of solar radii. The distance at which destruction occurs is greater for smaller asteroids, and their temperatures during perihelion passages are too low for evaporation to explain their disappearance. Although both bright and dark (high- and low-albedo) asteroids eventually break up, we find that low-albedo asteroids are more likely to be destroyed farther from the Sun, which explains the apparent excess of high-albedo near-Earth objects and suggests that low-albedo asteroids break up more easily as a result of thermal effects.
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Acknowledgements
Discussions with D. Nesvorný, K. Tsiganis and S. Jacobson as well as a review by A. Harris helped improve the manuscript. M.G. was funded by grant 137853 from the Academy of Finland and D.V. by grant GA13-01308S of the Czech Science Foundation. W.F.B. thanks NASA’s Near Earth Object Observation programme for supporting his work in this project. We acknowledge support by ESA via contract AO/1-7015/11/NL/LvH (Synthetic Generation of a NEO Population). CSC – IT Centre for Science Ltd, Finland, the Finnish Grid Infrastructure and the mesocentre SIGAMM at the Observatoire de la Côte d’Azur provided computational resources.
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M.G. conceived the disruption model. M.G., A.M. and W.F.B. carried out orbital integrations using code modified by D.V. and A.M. R.J., B.B., M.G. and E.B. estimated observational biases for CSS. M.G. developed the code for fitting model parameters and carried out the fits. M.D. provided expertise on the WISE albedo analysis. M.G. wrote the paper with input from all authors.
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The authors declare no competing financial interests.
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The code for orbital integrations, SWIFT, is available at https://www.boulder.swri.edu/~hal/downloads.
Supplementary information
Supplementary Information
This file contains a detailed description of the modelling approach describing the generation of steady-state orbit distributions, estimation of observational selection effects, and estimation of model parameters, Supplementary Figures 1–14 and Supplementary References. (PDF 2783 kb)
Debiased NEO orbital distribution
The fractional NEO orbit (a,e,i) distribution as a function of H when assuming a disruption at q⋆= 0.076 au. (MP4 79 kb)
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Granvik, M., Morbidelli, A., Jedicke, R. et al. Super-catastrophic disruption of asteroids at small perihelion distances. Nature 530, 303–306 (2016). https://doi.org/10.1038/nature16934
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DOI: https://doi.org/10.1038/nature16934
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