期刊
UNIVERSE
卷 8, 期 5, 页码 -出版社
MDPI
DOI: 10.3390/universe8050263
关键词
cosmology; galaxies; Tully-Fisher relation; gravitational transition
资金
- Hellenic Foundation for Research and Innovation [789]
Research suggests that a gravitational transition of the effective Newton's constant could lead to an increase in comet impact on the solar system, which may be linked to mass extinctions on Earth.
It has recently been suggested that a gravitational transition of the effective Newton's constant G(eff )by about 10%, 50-150 Myrs ago could lead to the resolution of both the Hubble crisis and the growth tension of the standard Lambda CDM model. Hints for such an abrupt transition with weaker gravity at times before the transition, have recently been identified in Tully-Fisher galactic mass-velocity data, and also in Cepheid SnIa calibrator data. Here we use Monte-Carlo simulations to show that such a transition could significantly increase (by a factor of 3 or more) the number of long period comets (LPCs) impacting the solar system from the Oort cloud (semi-major axis of orbits greater than or similar to 10(4) AU). This increase is consistent with observational evidence from the terrestrial and lunar cratering rates, indicating that the impact flux of kilometer sized objects increased by at least a factor of 2 over that last 100 Myrs compared to the long term average. This increase may also be connected with the Chicxulub impactor event that produced the Cretaceous-Tertiary (K-T) extinction of 75% of life on Earth (including dinosaurs) about 66 Myrs ago. We use Monte-Carlo simulations to show that for isotropic Oort cloud comet distribution with initially circular orbits, random velocity perturbations (induced e.g., by passing stars and/or galactic tidal effects), lead to a deformation of the orbits that increases significantly when G(eff )increases. A 10% increase in G(eff) leads to an increase in the probability of the comets to enter the loss cone and reach the planetary region (pericenter of less than 10 AU) by a factor that ranges from 5% (for velocity perturbation much smaller than the comet initial velocity) to more than 300% (for total velocity perturbations comparable with the initial comet velocity).
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