Diploma in Electric Propulsion Integration and eVTOL Architectures
About us Diploma in Electric Propulsion Integration and eVTOL Architectures
The Diploma in Electric Propulsion Integration and eVTOL Architectures explores the design and implementation of electric propulsion systems in vertical takeoff and landing (eVTOL) vehicles, integrating knowledge of electric motors, high-performance batteries, and flight control systems. It focuses on optimizing energy efficiency, thermal management, and safety, considering aeronautical regulations and market trends in urban air mobility (UAM).
The course provides an in-depth understanding of eVTOL architectures, including the design of propellers, rotor configurations, and power distribution systems. Simulation and analysis are addressed using computer-aided engineering (CAE) tools, with an emphasis on the application of certification standards and the challenges associated with autonomy and operational safety. Participants will gain hands-on experience in developing prototypes and evaluating the performance of electric propulsion systems.
Target keywords (naturally occurring in the text): electric propulsion, eVTOL, urban air mobility, electric motors, batteries, flight control systems, energy efficiency, thermal management, eVTOL architectures, aeronautical certification.
Diploma in Electric Propulsion Integration and eVTOL Architectures
- Format:
- Duration:
- Hours: 900 H
- Language:
- Credits:
- Registration date: 08-09-2026
- Strat date: 19-10-2026
- Available places: 9
1,295 $
Competencies and results
What you will learn
Who this program is for:
Diploma in Electric Propulsion Integration and eVTOL Architectures
9.9 Principles of Electric Propulsion for eVTOLs: Motors, Inverters, and Control.
9.9 eVTOL Architectures: Multirotor, Tilt-wing, Composite Configuration.
9.3 Power Systems and Thermal Management in eVTOLs.
9.4 Component Design and Selection: Batteries, Motors, ESCs.
9.5 Systems Integration: Avionics, Flight Control, Software.
9.6 Safety and Redundancy Considerations.
9.7 Performance Evaluation: Efficiency, Range, Noise.
9.8 Prototype Development and Flight Testing.
9.9 Future Trends and Challenges in eVTOL Electric Propulsion.
9.90 Case Study: Comparative Analysis of Different eVTOL Architectures.
9.9 Introduction to Rotor Modeling: Theory and Methods.
9.9 Blade Element Modeling: Aerodynamics and Structure. 9.3 Rotor performance analysis: thrust, power, efficiency.
9.4 Computational flow simulation (CFD) for rotors.
9.5 Rotor modeling in specialized software.
9.6 Sensitivity analysis and optimization of rotor design.
9.7 Simulation of different flight conditions.
9.8 Rotor stability and control analysis.
9.9 Rotor design and analysis: practical cases.
9.90 Model validation and comparison with experimental data.
3.9 eVTOL rotor design: selection of key parameters.
3.9 Aerodynamic analysis of rotors: blade element theory.
3.3 Design of airfoil profiles for rotors.
3.4 Structural analysis of rotors: loads, materials, and methods.
3.5 Rotor performance modeling and simulation.
3.6 Rotor design optimization for different missions. 3.7 Noise and Vibration Analysis in eVTOL Rotors
3.8 Rotor Integration with the Propulsion System
3.9 Rotor Failure and Reliability Analysis
3.90 Rotor Design: Case Studies and Practical Examples
4.9 Advanced Rotor Simulation Methods: CFD and Finite Element Analysis
4.9 Optimization Techniques: Genetic Algorithms, Response-Based Optimization
4.3 Rotor Design Sensitivity Analysis
4.4 Rotor Performance Optimization: Thrust, Efficiency, Noise
4.5 Structural Optimization of Rotors: Weight, Strength
4.6 Rotor Performance Simulation under Complex Flight Conditions
4.7 Aeroelastic Phenomena Simulation
4.8 Rotor Design and Optimization for Different eVTOL Applications
4.9 Design Uncertainty and Robustness Analysis 4.90 Application of simulation and optimization tools to real-world cases.
5.9 Fundamentals of electric propulsion for eVTOLs.
5.9 Design of electric motors for rotors.
5.3 Selection and sizing of inverters and controllers.
5.4 Modeling electric motor performance.
5.5 Integration of the electric motor with the rotor.
5.6 Modeling electric rotor performance.
5.7 Simulation of the eVTOL electric propulsion system.
5.8 Analysis of propulsion system efficiency.
5.9 Design of the battery system and thermal management.
5.90 Case studies: eVTOL electric propulsion systems.
6.9 Rotor design: principles and considerations.
6.9 Aerodynamic modeling of the rotor.
6.3 Rotor performance analysis: thrust, power, efficiency.
6.4 Optimization of rotor design. 6.5 Noise and Vibration Considerations
6.6 Rotor Design for Different eVTOL Missions
6.7 Rotor Performance Simulation Under Realistic Flight Conditions
6.8 Sensitivity Analysis and Rotor Design Optimization
6.9 Rotor Design and Analysis: Practical Examples
6.90 Comparison of Different Rotor Designs
7.9 Rotor Modeling: Concepts and Methods
7.9 Airflow Simulation Around the Rotor
7.3 Rotor-Wind Interaction Modeling
7.4 Rotor Simulation in Motion: Hovering and Translation
7.5 Rotor Performance Analysis: Thrust, Power, Efficiency
7.6 Rotor Vibration and Noise Simulation
7.7 Rotor Modeling with Specialized Software
7.8 Model Validation with Experimental Data 7.9 Sensitivity Analysis and Rotor Design Optimization
7.90 Comprehensive Rotor Design and Simulation: Practical Cases
8.9 Introduction to eVTOL Systems: Components and Architecture
8.9 Propulsion System Design: Rotors, Motors, Batteries
8.3 Flight Control System Design
8.4 Stability and Flight Control Analysis
8.5 eVTOL Airframe Design
8.6 Systems Integration: Avionics, Communications, Sensors
8.7 Safety and Certification Considerations
8.8 eVTOL Simulation and Performance Analysis
8.9 Failure and Reliability Analysis
8.90 Case Studies: Design and Analysis of Different eVTOL Systems
Capstone-type projects
Admissions, fees and scholarships
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