The cometary model of dust environments (ComMoDE)

Abstract The Cometary Model of Dust Environment (ComMoDE) is a software based on a time-efficient and highly flexible dust model to support the planning and operation of future cometary missions. The ESA Comet Interceptor mission further motivated the implementation of this model in dedicated software. Its goal is to perform a flyby at an as-yet unknown, dynamically new comet or interstellar object. This makes it difficult to constrain the expected dust environment. To address this issue, ComMoDE is specifically designed to allow for a large range of different parameters. The model is able to account for the solar radiation pressure, simple day-night asymmetries and variations in the dust production rate that may result from nucleus rotation. It is only valid outside of the acceleration region. The outputs of the model are the dust number densities for a chosen number of particle size bins, which are also used by the model to derive the number densities, fluxes, fluences and the total impacted mass along chosen flyby trajectories. ComMoDE has been tested extensively and is able to reproduce the measurements of the total impact mass on the Giotto spacecraft at comet 1P/Halley.

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Publication Details

Journal
CEAS Space Journal
Published
2025-08-13
DOI
https://doi.org/10.1007/s12567-025-00641-8
Primary Topic
Astro and Planetary Science
Type
article
Field-Weighted Citation Impact
0.00

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article

The cometary model of dust environments (ComMoDE)

Raphael Marschall, F. Cipriani, Nico Haslebacher, Philippe Reynier et al.
CEAS Space Journal
Astro and Planetary Science
article

The cometary model of dust environments (ComMoDE)

Raphael Marschall, F. Cipriani, Nico Haslebacher, Philippe Reynier, Omar Mokhtari, F. Johansson, N. Thomas, Rocco Arpa
article en

Abstract

Abstract The Cometary Model of Dust Environment (ComMoDE) is a software based on a time-efficient and highly flexible dust model to support the planning and operation of future cometary missions. The ESA Comet Interceptor mission further motivated the implementation of this model in dedicated software. Its goal is to perform a flyby at an as-yet unknown, dynamically new comet or interstellar object. This makes it difficult to constrain the expected dust environment. To address this issue, ComMoDE is specifically designed to allow for a large range of different parameters. The model is able to account for the solar radiation pressure, simple day-night asymmetries and variations in the dust production rate that may result from nucleus rotation. It is only valid outside of the acceleration region. The outputs of the model are the dust number densities for a chosen number of particle size bins, which are also used by the model to derive the number densities, fluxes, fluences and the total impacted mass along chosen flyby trajectories. ComMoDE has been tested extensively and is able to reproduce the measurements of the total impact mass on the Giotto spacecraft at comet 1P/Halley.

CEAS Space Journal
CEA CESTA (FR), Centre National de la Recherche Scientifique (FR), Optima Neuroscience (United States) (US), Observatoire de la Côte d’Azur (FR), European Space Research and Technology Centre (NL)
National Science Foundation, University of Bern, European Space Agency, Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung
Openalex Percentile: Top 85%
Astro and Planetary Science
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