ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F26%3A0200073" target="_blank" >RIV/00216305:26210/26:0200073 - isvavai.cz</a>
Result on the web
<a href="https://www.engmech.cz/improc/2024/110.pdf" target="_blank" >https://www.engmech.cz/improc/2024/110.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.21495/em2024-110" target="_blank" >10.21495/em2024-110</a>
Alternative languages
Result language
angličtina
Original language name
ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN
Original language description
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.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
—
OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
—
Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2024
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů