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In the current work, an analysis for the initial aerodynamic assessment of a small sized quadcopter drone propeller is presented, focusing on the drone aerodynamic characteristics optimization. The objective of the work is to design and construct from scratch a quadcopter drone, in order to participate to the UAS Challenge 2020 student competition (www.imeche.org/events/challenges/uas-challenge). The study of the quadcopter design and construction is carried out by the Democritus Aeronauticaldoi:10.3303/cet1976031 doaj:4afdf3d91d4e4e2dab2838d96f722d82 fatcat:h4isuk2glfbdxdnssmg2r5d7nm