Flying in the atmosphere of selected bodies of our solar system

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F25%3A00387560" target="_blank" >RIV/68407700:21220/25:00387560 - 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

Flying in the atmosphere of selected bodies of our solar system

Popis výsledku v původním jazyce

Our solar system contains several bodies (i.e., some of the planets and the moons) with atmosphere suitable for flying. Motivation for the design of machines flying in the atmosphere of these bodies is basically scientific. They can be used for investigation of the atmosphere, topography tasks or for the sample return on the Earth. This paper is focused on the investigation of the analysis of the possibility of the flight for both fixed-wing and rotary-wing aircraft. Analytical approximation of the atmospheric properties including local gravity acceleration is used for every selected body. Aircraft performance is estimated for both rotary- and fixed-wing configurations and various missions (e.g., photographic missions or atmospheric research missions). Energy consumption is calculated for every mission (various propulsion systems are considered), and the results are discussed.

Název v anglickém jazyce

Flying in the atmosphere of selected bodies of our solar system

Popis výsledku anglicky

Our solar system contains several bodies (i.e., some of the planets and the moons) with atmosphere suitable for flying. Motivation for the design of machines flying in the atmosphere of these bodies is basically scientific. They can be used for investigation of the atmosphere, topography tasks or for the sample return on the Earth. This paper is focused on the investigation of the analysis of the possibility of the flight for both fixed-wing and rotary-wing aircraft. Analytical approximation of the atmospheric properties including local gravity acceleration is used for every selected body. Aircraft performance is estimated for both rotary- and fixed-wing configurations and various missions (e.g., photographic missions or atmospheric research missions). Energy consumption is calculated for every mission (various propulsion systems are considered), and the results are discussed.

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

74-77

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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