Santos, Dino Lincoln FigueirôaCosta, Andrielly Santiago Lima da2024-07-162024-07-162024-06-17Costa, Andrielly Santiago Lima da. Design de sistema de emergência para aeronaves remotamente pilotadas: estudo de caso do SPACEVANT. 2024. 60 f. Trabalho de Conclusão de Curso (Graduação em Design) - Departamento de Design, Universidade Federal do Rio Grande do Norte, Natal, 2024.https://repositorio.ufrn.br/handle/123456789/58792In the present study, the design of an aerodynamic fairing housing a cylindrical parachute deployment device, along with all the embedded technology, was addressed, using the SPACEVANT from CLBI as a reference. An emergency system is crucial in remotely piloted aircraft as it ensures operational safety, protects third parties, and preserves the integrity of the aircraft. By autonomously detecting and responding to failures or emergencies, the system allows the aircraft to react quickly, preventing accidents. Given the importance of an emergency system and the need to design a fairing that minimally impacts the drone's aerodynamics, a shell based on the Sears-Haack body, which generates the least fuselage drag, was developed. The Aerospace Design methodology was used to conceive an emergency device with an optimized design for reducing the drone's drag force. The design of this new aerodynamic fairing device resulted in a 6.72% increase in the vehicle's aerodynamic drag.Carenagem aerodinâmicasistema de emergênciaVANTSears-Haackdesign aeroespacialbachelorThesis