Dear Sir or Madam, we are an early-stage startup working on a hybrid VTOL UAV concept and are currently preparing material for an initial technical feasibility discussion with a university. For this purpose, we are looking for support with a conceptual three-view layout (top / side / front), potentially complemented by one or two simple sectional views. Scope is strictly limited to: conceptual geometry and proportions placement of main components (lift fan, batteries, generator, landing gear, tanks) consistency between views Explicitly excluded from scope: detailed or production-level design structural analysis (FEM) CFD certification or compliance activities This work is intended purely as a discussion and feasibility basis, not as a finalized design. As a startup project, we are working with a limited budget and are therefore interested in a lean, cost-efficient approach suitable for an early concept phase. All available technical inputs, sketches, mass data and references will be provided to minimize effort on your side. We would be grateful for your feedback on whether this scope could be feasible for you and, if so, what level of effort and timeline you would consider appropriate. Kind regards I'm looking for a detailed, conceptual 3-view CAD layout for an early-stage UAV delivery project. The UAV will primarily operate in mixed environments and needs to have a high payload capacity. Ideal Skills & Experience: - Proficiency in CAD software (AutoCAD, SolidWorks, etc.) - Experience in UAV design and development - Understanding of payload capacity requirements - Knowledge of design for mixed environmental operation