Hello,
After read project requirements, I understood that these specifications demand a comprehensive approach to drone design, load capacity analysis, power system optimization, and flight time extension.
First, I need to analyze the design constraints and load distribution to ensure structural integrity and flight stability. Simultaneously, we'll evaluate power requirements and distribution to determine the feasibility of using 8x) 21.5 HP gas engines. Aerodynamic considerations will guide propeller selection and efficiency optimization to maximize thrust output while minimizing energy consumption. Additionally, battery capacity and management systems will be evaluated to achieve the desired flight time.
In terms of tools, we'll leverage CAD software for 3D modeling and structural analysis, computational fluid dynamics (CFD) simulations for aerodynamic optimization, and power system modeling software for efficiency analysis. Physical prototyping and testing will validate simulation results and fine-tune the design.
I'd like to know about etc...
What are the specific dimensions and weight distribution of the payload?
Are there any constraints or regulations regarding drone size, weight, or flight characteristics?
What are the environmental conditions the drone will operate in (e.g., altitude, temperature, wind)?
Waiting for your reply.
Best Regards,