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HAVRAN, E.
Originální název
ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN
Anglický název
Druh
Stať ve sborníku mimo WoS a Scopus
Originální abstrakt
An analysis of Mars rotary wing aircraft was done, regarding a quadcopter design. A mission profile was proposed, that could be generalized to multiple mission goals. Energy requirements for such a mission were computed and then a mass sizing of the drone was calculated. This resulted in various design points of Mars drones, in accordance with what initial conditions (for example rotor count) were chosen. Next, using blade element momentum theory, an analytical model of the rotors was calculated and implemented to the drone, so as to create a conceptual design for later research and development use.
Anglický abstrakt
Klíčová slova
Mars drone, conceptual design, mass sizing, blade element momentum theory
Klíčová slova v angličtině
Autoři
Vydáno
16.05.2024
Nakladatel
Institute of Thermomechanics of the Czech Academy of Sciences
Místo
Praha
Periodikum
Engineering Mechanics
Stát
Česká republika
Strany od
110
Strany do
113
Strany počet
4
URL
https://www.engmech.cz/improc/2024/110.pdf
BibTex
@inproceedings{BUT200073, author="Edmund {Havran}", title="ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN", year="2024", journal="Engineering Mechanics", pages="110--113", publisher="Institute of Thermomechanics of the Czech Academy of Sciences", address="Praha", doi="10.21495/em2024-110", issn="1805-8248", url="https://www.engmech.cz/improc/2024/110.pdf" }