Detail VaV (200073) ▪ FSI VUT v Brně

Anglický název

ANALYTICAL INVESTIGATION OF MARS DRONE CONCEPTUAL DESIGN

Typ

Stať ve sborníku mimo WoS a Scopus

Jazyk

en

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.

Klíčová slova anglicky

Mars drone, conceptual design, mass sizing, blade element momentum theory

Vydáno

2024-05-16

Nakladatel

Institute of Thermomechanics of the Czech Academy of Sciences

Místo

Praha

Časopis

Engineering Mechanics

Strany od–do

110–113

Počet stran

4

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"
}