Excited to share the results of our two-month effort in the Aircraft Conceptual Design course. Our team (Gabriele Di Natale , Federica Pino, Matteo Bonadonna , Matteo Corona , Tanguy Maillach , Charlotte Grégoire ) embarked on designing a state-of-the-art MALE UAV, focused on designing a state-of-the-art MALE UAV, addressing two main requirements: "First level requirements (Regulations)" based on STANAG 4671, and "Second level requirements (Project requirements)".
Key project requirements we aimed to meet: Endurance comparable to X-47B, Carrier operations capable, Internal volume suitable for state-of-the-art reconnaissance, MTOW comparable to MQ-4C Triton, Cost per unit comparable to Global Hawk.
Despite successfully addressing all regulatory and project requirements, this design is a theoretical exercise requiring a more extended timeframe of about 5 years for actual implementation.
Abstract of the Report:
In this report, we journey through the realm of aerospace technology, focusing on a marvel of modern innovation - the Unmanned Aerial Vehicle (UAV). This project involved creating a conceptual design for a Medium Altitude Long Endurance (MALE) UAV, integrating the latest advancements in technology while ensuring compliance with stringent regulatory standards.
We begin with an Introduction to UAVs, exploring their various classifications and the importance of stealthiness, including acoustic, infrared, visual, and radar stealth. The Initial Sizing chapter covers the fundamental calculations necessary to define the basic parameters of our UAV, such as weight and performance estimates.
In the Aerodynamics section, we delve into the design of the airfoil and wing, emphasizing the importance of achieving optimal lift-to-drag ratios. This is followed by Structures, where we detail the materials and construction methods used to ensure both strength and lightweight characteristics.
Propulsion examines the various aeronautical propulsion technologies, focusing on the selection and integration of an appropriate engine. Avionics covers the autonomous navigation and flight control systems essential for modern UAV operations.
We also address Systems Integration, discussing the integration of various subsystems such as fuel, electrical, and landing gear. Weight and Balance analyses are critical for ensuring the stability and control of the UAV.
The Performance chapter evaluates the UAV's capabilities in different flight conditions, while Mission Analysis assesses its operational effectiveness in various scenarios.
Finally, we conclude with Cost Analysis, providing an estimate of the production and operational costs, and Conclusions, summarizing the project's achievements and the potential future work required to bring this concept to reality.
Thank you to everyone who contributed to this ambitious project! #AerospaceEngineering #UAV #Innovation #BWB
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