ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN
Identifikátory výsledku
Kód výsledku v 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>
Výsledek na webu
<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>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN
Popis výsledku anglicky
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.
Klasifikace
Druh
O - Ostatní výsledky
CEP obor
—
OECD FORD obor
20304 - Aerospace engineering
Návaznosti výsledku
Projekt
—
Návaznosti
S - Specificky vyzkum na vysokych skolach
Ostatní
Rok uplatnění
2024
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů