CourseAerospace, UAM, Drones & Space Applications open

Course on hybrid electric systems in aviation

Online course of 300 hours in hybrid-electric systems in aviation. 6 modules covering propulsion electrification, powertrain components, high-voltage electrical systems, energy management and control and electric propulsion certification with an assigned technical tutor.

Duration3 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute certificate
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Learning outcomes

What you will be able to do

01

Understand hybrid and electric propulsion architectures.

02

Select and size the components of an electric powertrain.

03

Design high-voltage electrical systems suited to the aerospace environment.

04

Develop energy management strategies for a mission profile.

05

Know the certification framework for electric propulsion.

06

Evaluate mass, efficiency and emissions against conventional solutions.

07

Design a hybrid-electric propulsion system for a specific aircraft.

Profile

Who it's for

  • Electric propulsion engineers.
  • Power electronics engineers moving into aerospace.
  • Aircraft electrical systems engineers.
  • Energy management engineers.
  • Propulsion certification engineers.
  • Sustainable aviation researchers.
  • Engineering or science graduates seeking to join aircraft manufacturers.
Standards & tools

What you'll work with

  • EASA SC E-19 (special condition for electric and hybrid propulsion systems)
  • EASA CS-23 (certification specifications for normal-category aeroplanes)
  • MIL-STD-704F (aircraft electric power characteristics)
  • RTCA DO-160G / EUROCAE ED-14G (environmental conditions and test procedures for airborne equipment)
  • ASTM F3338 (design of electric propulsion units for aircraft)
  • RTCA DO-311A (rechargeable lithium battery systems)
  • SAE ARP4761A / EUROCAE ED-135 (safety assessment process for civil aircraft systems)
  • SAE AS50881 (aerospace vehicle wiring)
  • MATLAB/Simulink
  • Simscape Electrical
  • PLECS
  • Ansys Motor-CAD
  • GasTurb
Syllabus

6 modules

  1. 1.1Environmental and economic drivers
  2. 1.2All-electric architectures
  3. 1.3Series, parallel and turboelectric hybrids
  4. 1.4Partial and mild hybridisation
  5. 1.5Relevant demonstrator programmes
  6. 1.6Energy density and specific power
  7. 1.7Endurance and range limitations
  8. 1.8Impact on aircraft design
  9. 1.9Roadmap for regional aviation
  10. 1.10Case study: architectures for a 19-seat aircraft
  1. 2.1Permanent-magnet synchronous electric motors
  2. 2.2Superconducting electrical machines
  3. 2.3Inverters and power converters
  4. 2.4SiC and GaN semiconductors
  5. 2.5Turbine-coupled generators
  6. 2.6Battery and supercapacitor storage
  7. 2.7Fuel cells as a power source
  8. 2.8Cables, connectors and protection
  9. 2.9Mass and efficiency of each component
  10. 2.10Workshop: powertrain efficiency chain
  1. 3.1DC voltage levels
  2. 3.2Partial discharge and corona effect at altitude
  3. 3.3Insulation and clearances at low pressure
  4. 3.4Arc protection
  5. 3.5Power quality under MIL-STD-704F
  6. 3.6Distribution and solid-state contactors
  7. 3.7Grounding and electromagnetic compatibility
  8. 3.8Thermal management of electronics
  9. 3.9Safety of maintenance personnel
  10. 3.10Lab: partial discharge analysis of a cable
  1. 4.1Power-split strategies
  2. 4.2Rule-based and optimisation-based control
  3. 4.3State-of-charge management during the mission
  4. 4.4Energy trajectory optimisation
  5. 4.5Motor and inverter control
  6. 4.6Degraded modes and failures
  7. 4.7Integration with flight management
  8. 4.8Predictive energy algorithms
  9. 4.9Crew interface
  10. 4.10Practical exercise: power-split strategy over a mission profile
  1. 5.1Special Condition SC E-19
  2. 5.2Applicable CS-23 requirements
  3. 5.3EASA means of compliance
  4. 5.4Powerplant safety analysis
  5. 5.5Durability and endurance testing
  6. 5.6Battery fire protection
  7. 5.7Environmental compatibility under DO-160G
  8. 5.8ASTM standards for electric propulsion
  9. 5.9Certification experience with light aircraft
  10. 5.10Case study: compliance matrix for an electric engine
  1. 6.1Mission and aircraft requirements
  2. 6.2Selection of the hybrid architecture
  3. 6.3Component sizing
  4. 6.4System model and simulation
  5. 6.5Energy management strategy
  6. 6.6Mass and emissions assessment
  7. 6.7Preliminary safety analysis
  8. 6.8Comparison with conventional propulsion
  9. 6.9Report and presentation
  10. 6.10Final project: final review with the tutor
Methodology, software & labs

How you'll learn

100% online training on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. There are no fixed timetables: you progress at your own pace within the intake, so the programme fits around your job.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is MATLAB/Simulink, Simscape Electrical, PLECS, Ansys Motor-CAD and GasTurb, in free, academic or evaluation versions. Exercises are based on real procedures: sizing hybrid powertrains, simulating energy management strategies and analysing high-voltage insulation. Assessment is continuous by module, plus the final capstone project.

Standards covered: EASA SC E-19, EASA CS-23, MIL-STD-704F, RTCA DO-160G / EUROCAE ED-14G, ASTM F3338, RTCA DO-311A, SAE ARP4761A / EUROCAE ED-135, SAE AS50881.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of EASA SC E-19, EASA CS-23 and MIL-STD-704F applied to real cases, not as a theoretical annex.
Industry software:MATLAB/Simulink, Simscape Electrical, PLECS, Ansys Motor-CAD, GasTurb, in free, academic or evaluation versions.
Final project:a hybrid-electric propulsion system for a specific aircraft, from architecture selection to simulation and preliminary safety analysis, reviewed by your tutor.
Flexible format:100% online, no fixed timetables, compatible with full-time work.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Requirements and architecture
Define mission and aircraft requirements and select the hybrid architecture.
Component sizing
Size the motors, converters, generators and energy storage.
System simulation
Model and simulate the system with an energy management strategy.
Mass, emissions and safety
Assess mass and emissions and carry out a preliminary safety analysis.
Final project
A documented hybrid-electric design compared with conventional propulsion, reviewed with your tutor.
Career opportunities

Where this takes you

Electric Propulsion EngineerPower Electronics EngineerAircraft Electrical Systems EngineerEnergy Management EngineerPropulsion Certification EngineerSustainable Aviation Researcher
Admissions & scholarships

Requirements

  • No prior qualification is required.
  • An internet connection and a computer capable of running the programme software.
  • English sufficient to read technical standards.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

FAQ

Frequently asked questions

The programme totals 300 hours over 3 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with MATLAB/Simulink, Simscape Electrical, PLECS, Ansys Motor-CAD, GasTurb, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute certificate, awarded on passing the continuous assessment and the final project. It is SEIUM's own qualification, not an official state degree; its recognition depends on the programme completed and the regulations of each country.

Yes. Modules passed are recognised in a higher programme in the same area (postgraduate diploma or master's). Ask about the recognition policy when you enrol.

No prior qualification is required; you need an internet connection, a computer able to run the programme software and enough English to read technical standards.

Start dates are set by SEIUM's faculty for each intake. Our admissions team will confirm the next available date when you apply.

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