Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters

Using the gas drag by sublimating cometary surface ices for the acceleration of dust particles and deceleration by the gravity field of the nucleus combined with basic laws of mechanics, the sizes, velocities, and number densities of escaping particles are calculated and evaluated with respect to th...

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Main Authors: Uwe Fink, Walter Harris, Lyn Doose, Kat Volk, Laura Woodney, Tony Farnham, Maria Womack
Format: Article
Language:English
Published: IOP Publishing 2021-01-01
Series:The Planetary Science Journal
Subjects:
Online Access:https://doi.org/10.3847/PSJ/ac09f0
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author Uwe Fink
Walter Harris
Lyn Doose
Kat Volk
Laura Woodney
Tony Farnham
Maria Womack
author_facet Uwe Fink
Walter Harris
Lyn Doose
Kat Volk
Laura Woodney
Tony Farnham
Maria Womack
author_sort Uwe Fink
collection DOAJ
description Using the gas drag by sublimating cometary surface ices for the acceleration of dust particles and deceleration by the gravity field of the nucleus combined with basic laws of mechanics, the sizes, velocities, and number densities of escaping particles are calculated and evaluated with respect to the hazard assessment of comet–spacecraft flybys and encounters. We find good agreement between our analytical method and the more elaborate and precise DSMC calculations, but, being simpler, our method can more easily be used to explore a wide range of cometary conditions and can be more easily scaled to specific comets with different nucleus sizes, masses, and gravity potentials and various gas and dust production rates. Our analytical method is applied to outbursts expanding into a cone of ∼60°, where the gas density falls off with height from the surface rather than radial distance from the center of a uniformly outgassing nucleus. In this scenario, larger dust particles can be ejected and attain ballistic trajectories, go into orbit, or escape from the nucleus, thus being potentially more hazardous to a spacecraft. Sample calculations are carried out for potential dust outbursts for the highly active Centaur/Comet 29P/Schwassmann-Wachmann 1 for various assumed active areas and dust particle size distributions. Particle velocity ranges for ballistic trajectories, orbiting particles, and particles escaping into the coma are presented. These calculations are used to estimate the coma particle number densities during outbursts to get an assessment of the hazards and required mitigation for a flyby or orbiting space mission.
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spelling doaj.art-20cb4dc5e6e0425187dbbb1260fc2ec52024-02-03T07:27:39ZengIOP PublishingThe Planetary Science Journal2632-33382021-01-012415410.3847/PSJ/ac09f0Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet EncountersUwe Fink0Walter Harris1https://orcid.org/0000-0002-8378-4503Lyn Doose2https://orcid.org/0000-0003-4253-0950Kat Volk3https://orcid.org/0000-0001-8736-236XLaura Woodney4https://orcid.org/0000-0002-0004-7381Tony Farnham5https://orcid.org/0000-0002-4767-9861Maria Womack6https://orcid.org/0000-0003-4659-8653Lunar and Planetary Laboratory, University of Arizona , Tucson, AZ 85721, USALunar and Planetary Laboratory, University of Arizona , Tucson, AZ 85721, USALunar and Planetary Laboratory, University of Arizona , Tucson, AZ 85721, USALunar and Planetary Laboratory, University of Arizona , Tucson, AZ 85721, USACalifornia State University San Bernardino, Department of Physics, San Bernardino, CA 92407, USADepartment of Astronomy, University of Maryland , College Park, MD 20742, USADepartment of Physics, University of Central Florida , Orlando, FL 32816, USAUsing the gas drag by sublimating cometary surface ices for the acceleration of dust particles and deceleration by the gravity field of the nucleus combined with basic laws of mechanics, the sizes, velocities, and number densities of escaping particles are calculated and evaluated with respect to the hazard assessment of comet–spacecraft flybys and encounters. We find good agreement between our analytical method and the more elaborate and precise DSMC calculations, but, being simpler, our method can more easily be used to explore a wide range of cometary conditions and can be more easily scaled to specific comets with different nucleus sizes, masses, and gravity potentials and various gas and dust production rates. Our analytical method is applied to outbursts expanding into a cone of ∼60°, where the gas density falls off with height from the surface rather than radial distance from the center of a uniformly outgassing nucleus. In this scenario, larger dust particles can be ejected and attain ballistic trajectories, go into orbit, or escape from the nucleus, thus being potentially more hazardous to a spacecraft. Sample calculations are carried out for potential dust outbursts for the highly active Centaur/Comet 29P/Schwassmann-Wachmann 1 for various assumed active areas and dust particle size distributions. Particle velocity ranges for ballistic trajectories, orbiting particles, and particles escaping into the coma are presented. These calculations are used to estimate the coma particle number densities during outbursts to get an assessment of the hazards and required mitigation for a flyby or orbiting space mission.https://doi.org/10.3847/PSJ/ac09f0ComaeSpace probes
spellingShingle Uwe Fink
Walter Harris
Lyn Doose
Kat Volk
Laura Woodney
Tony Farnham
Maria Womack
Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters
The Planetary Science Journal
Comae
Space probes
title Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters
title_full Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters
title_fullStr Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters
title_full_unstemmed Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters
title_short Dust Outburst Dynamics and Hazard Assessment for Close Spacecraft–Comet Encounters
title_sort dust outburst dynamics and hazard assessment for close spacecraft comet encounters
topic Comae
Space probes
url https://doi.org/10.3847/PSJ/ac09f0
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