Modelling cometary meteoroid stream traverses of the Martian Moons eXploration (MMX) spacecraft en route to Phobos

dc.contributor.authorKrüger, Harald
dc.contributor.authorKobayashi, Masanori
dc.contributor.authorStrub, Peter
dc.contributor.authorMoragas-Klostermeyer, Georg
dc.contributor.authorSommer, Maximilian
dc.contributor.authorKimura, Hiroshi
dc.contributor.authorGrün, Eberhard
dc.contributor.authorSrama, Ralf
dc.date.accessioned2023-06-01T08:06:00Z
dc.date.available2023-06-01T08:06:00Z
dc.date.issued2021de
dc.date.updated2023-03-28T08:49:18Z
dc.description.abstractThe Martian Moons Exploration (MMX) spacecraft is a JAXA mission to Mars and its moons Phobos and Deimos. MMX will be equipped with the Circum-Martian Dust Monitor (CMDM) which is a newly developed light-weight (650g) large area (1m2) dust impact detector. Cometary meteoroid streams (also referred to as trails) exist along the orbits of comets, forming fine structures of the interplanetary dust cloud. The streams consist predominantly of the largest cometary particles (with sizes of approximately 100μm to 1 cm) which are ejected at low speeds and remain very close to the comet orbit for several revolutions around the Sun. The Interplanetary Meteoroid Environment for eXploration (IMEX) dust streams in space model is a new and recently published universal model for cometary meteoroid streams in the inner Solar System. We use IMEX to study the detection conditions of cometary dust stream particles with CMDM during the MMX mission in the time period 2024 to 2028. The model predicts traverses of 12 cometary meteoroid streams with fluxes of 100μm and bigger particles of at least 10-3m-2day-1 during a total time period of approximately 90 days. The highest flux of 0.15m-2day-1 is predicted for comet 114P/Wiseman-Skiff in October 2026. With its large detection area and high sensitivity CMDM will be able to detect cometary meteoroid streams en route to Phobos. Our simulation results for the Mars orbital phase of MMX also predict the occurrence of meteor showers in the Martian atmosphere which may be observable from the Martian surface with cameras on board landers or rovers. Finally, the IMEX model can be used to study the impact hazards imposed by meteoroid impacts onto large-area spacecraft structures that will be particularly necessary for crewed deep space missions.en
dc.description.sponsorshipProjekt DEALde
dc.identifier.issn1880-5981
dc.identifier.other1849807531
dc.identifier.urihttp://nbn-resolving.de/urn:nbn:de:bsz:93-opus-ds-131198de
dc.identifier.urihttp://elib.uni-stuttgart.de/handle/11682/13119
dc.identifier.urihttp://dx.doi.org/10.18419/opus-13100
dc.language.isoende
dc.relation.uridoi:10.1186/s40623-021-01412-5de
dc.rightsinfo:eu-repo/semantics/openAccessde
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/de
dc.subject.ddc620de
dc.titleModelling cometary meteoroid stream traverses of the Martian Moons eXploration (MMX) spacecraft en route to Phobosen
dc.typearticlede
ubs.fakultaetLuft- und Raumfahrttechnik und Geodäsiede
ubs.fakultaetFakultätsübergreifend / Sonstige Einrichtungde
ubs.institutInstitut für Raumfahrtsystemede
ubs.institutFakultätsübergreifend / Sonstige Einrichtungde
ubs.publikation.seiten13de
ubs.publikation.sourceEarth, planets and space 73 (2021), No. 93de
ubs.publikation.typZeitschriftenartikelde

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