Investigation of low altitude orbits around selected bodies of the solar system

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F25%3A00387540" target="_blank" >RIV/68407700:21220/25:00387540 - isvavai.cz</a>

Výsledek na webu

<a href="https://compmech.kme.zcu.cz/download/proceedings/CM2025_Conference_Proceedings.pdf" target="_blank" >https://compmech.kme.zcu.cz/download/proceedings/CM2025_Conference_Proceedings.pdf</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Investigation of low altitude orbits around selected bodies of the solar system

Popis výsledku v původním jazyce

The need for better understanding of operations in proximity to other planets becomes more important with the amount of space missions increasing. Many possible mission tasks, ranging from surface mapping to sample retrieval, must be supported by satellites operating on lowest possible orbits. This paper focuses on these orbits in proximity to various planets and moons of the Solar system. Firstly, a simplified atmospheric model for planets and moons of the Solar System is established. This is then used for the selection of bodies of interest by means of the investigation of the drag and its influence on the orbit. This allows lowest acceptable orbits to be established under variety of circumstances. These can range from temporary orbits awaiting return of the away mission, e.g. manned or unmanned sample retrieval mission, long term orbits with low orbital station-keeping costs or planned disposal and minimization of space debris.

Název v anglickém jazyce

Investigation of low altitude orbits around selected bodies of the solar system

Popis výsledku anglicky

The need for better understanding of operations in proximity to other planets becomes more important with the amount of space missions increasing. Many possible mission tasks, ranging from surface mapping to sample retrieval, must be supported by satellites operating on lowest possible orbits. This paper focuses on these orbits in proximity to various planets and moons of the Solar system. Firstly, a simplified atmospheric model for planets and moons of the Solar System is established. This is then used for the selection of bodies of interest by means of the investigation of the drag and its influence on the orbit. This allows lowest acceptable orbits to be established under variety of circumstances. These can range from temporary orbits awaiting return of the away mission, e.g. manned or unmanned sample retrieval mission, long term orbits with low orbital station-keeping costs or planned disposal and minimization of space debris.

Druh

D - Stať ve sborníku

CEP obor

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OECD FORD obor

20304 - Aerospace engineering

Projekt

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Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2025

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

PROCEEDINGS OF COMPUTATIONAL MECHANICS 2025

ISBN

978-80-261-1254-9

ISSN

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e-ISSN

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Počet stran výsledku

4

Strana od-do

45-48

Název nakladatele

Západočeská univerzita v Plzni

Místo vydání

Plzeň

Místo konání akce

Srní

Datum konání akce

3. 11. 2025

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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