A model of the heliocentric dust ring on Venus orbit
Ariane Courtot, Mark Millinger
TL;DR
This work builds a dynamical model of the circumsolar dust ring on Venus’s orbit to quantify particle distribution, velocity, and density and to estimate spacecraft impact risk. It employs two initialization schemes (IC1 and IC2) and long multi-millennial integrations with a Radau integrator, including non-gravitational forces, to reveal ring evolution and its implications for a mission like BepiColombo. The model indicates the ring persists for at least several millennia, remains concentrated near Venus’s orbit, and exhibits a modest debris flux that is comparable to the interplanetary background, signifying a low risk for gravity-assisted spacecraft. The study also discusses major uncertainties and outlines pathways for refinement with future observations and alternative size-distribution models, underscoring the need for data to constrain azimuthal variations and the ring’s origin.
Abstract
A heliocentric dust ring on Venus orbit was discovered following observations by the Helios spacecraft, and then confirmed thanks to observations by STEREO and the Parker Solar Probe. The impact risk it poses needs to be evaluated for any spacecraft crossing the ring. This study aims to provide a first model of the dust ring, in terms of distribution of particles (including size distribution), velocity, density of the ring, and deduce a first estimation of the impact risk to spacecrafts crossing the ring. We seek to describe the orbits of dust particles in the ring. We explore a first simple model, that leads us to propose a second, more elaborate, model. This model is then populated by particles that we integrate for 2000 years. We demonstrate that the dust ring will persist over the next 2000 years, only slightly extending radially and perpendicularly to the Venus orbital plane. We show that particles tend to accumulate at Venus orbit, but that along it the differences in density is negligible. We compute the number of particles we can expect to find in the ring. Finally, as an example, we apply this model to Bepi-Colombo to obtain a first estimate of the impact flux in function of radius and mass, for radii between 2 $μ$m and 2 cm (i.e. for masses between 10^-2 kg and 10^-14 kg). We also present the impact velocity and direction of impacts with respect to Bepi-Colombo. We are able to conclude that the ring seems to present a low risk for spacecrafts using Venus as a gravity assist.
