Master’s in MBSE for Aerospace Engineering
Online master's programme of 1,900 hours in MBSE for aerospace, structured in 12 modules covering SysML v1 and v2, MBSE methodologies, mission analysis, model-based requirements, architecture, simulation, safety, verification and organisational adoption, with an assigned technical tutor.
Take the controls.
Run a real engineering trade-off from this field. Move the sliders, watch the model react in real time and beat the challenge.
What you will be able to do
Understand the fundamentals of systems engineering and the MBSE approach.
Model aerospace systems with SysML v1 and v2.
Apply MBSE methodologies such as Arcadia, OOSEM or MagicGrid.
Manage requirements and traceability from the model.
Develop functional and physical architectures.
Integrate analysis, simulation and safety into the model.
Plan the implementation of MBSE in an organisation.
Who it's for
- MBSE systems engineers looking to consolidate their modelling practice in aerospace programmes.
- Aerospace systems architects who want a rigorous model-based workflow.
- Requirements engineers moving from document-based to model-based traceability.
- Model-based safety engineers working with ARP4761A.
- Systems engineering managers leading MBSE adoption.
- MBSE consultants advising aerospace, space and defence clients.
- Engineering or science graduates aiming to join aeronautical manufacturers.
What you'll work with
- ISO/IEC/IEEE 15288:2023 (system life cycle processes)
- ISO/IEC/IEEE 42010 (architecture description)
- OMG SysML v1.7 (systems modelling language)
- OMG SysML v2 (next-generation systems modelling language)
- SAE ARP4754A (development of civil aircraft and systems)
- ECSS-E-ST-10C (space systems engineering general requirements)
- ECSS-E-TM-10-25A (engineering design model data exchange)
- NASA/SP-2016-6105 Systems Engineering Handbook (NASA systems engineering practice)
- Cameo Systems Modeler
- Capella
- IBM Rhapsody
- MATLAB/Simulink
- Enterprise Architect
12 modules · 1900 h
1.1System life cycle under ISO/IEC/IEEE 152881.2The V-model and its variants1.3Document-based systems engineering1.4Limitations of the document-centric approach1.5MBSE concepts and the authoritative model1.6INCOSE MBSE initiatives1.7ESA and NASA project phases1.8Management of complex interfaces1.9Benefits of MBSE in aeronautical programmes1.10Case study: diagnosis of a document-based process
2.1BDD and IBD block diagrams2.2Requirement diagrams2.3Use case diagrams2.4Activity diagrams2.5Sequence diagrams2.6State machines2.7Parametric diagrams and constraints2.8Profiles and stereotypes2.9Modelling good practice2.10Lab: SysML model of a landing gear system
3.1Motivation for SysML v23.2Textual and graphical syntax3.3Standardised SysML v2 API3.4Definition and usage model3.5Variability in SysML v23.6Migration from SysML v13.7Tools compatible with SysML v23.8KerML as the base language3.9Interoperability between tools3.10Practical exercise: textual model of a function in SysML v2
4.1Arcadia method and Capella4.2INCOSE OOSEM4.3Dassault MagicGrid methodology4.4IBM Harmony SE4.5Comparison of methodologies4.6Selection according to the organisation4.7NAF and UAF architecture frameworks4.8Adaptation to the aerospace sector4.9Combination with agile processes4.10Case study: methodology selection for a satellite programme
5.1Stakeholder needs5.2Concept of operations5.3System operational scenarios5.4System capabilities5.5Context analysis5.6System modes and states5.7Measures of effectiveness5.8Mission trade-offs5.9Validation with stakeholders5.10Workshop: operational analysis of an observation mission
6.1Capturing requirements in the model6.2Derive and satisfy relationships6.3Traceability between requirements and architecture6.4Integration with DOORS and Polarion6.5Requirements quality using INCOSE guidance6.6Interface requirements6.7Verification of requirements in the model6.8Management of requirement changes6.9Automated impact analysis6.10Practical exercise: requirements traceability in Cameo
7.1Functional decomposition of the system7.2Allocation of functions to components7.3Definition of the logical architecture7.4Definition of the physical architecture7.5Interfaces and flows7.6Software and hardware architecture7.7Aerospace architecture patterns7.8Evaluation of alternatives7.9Documentation generated from the model7.10Lab: physical architecture of a fuel system
8.1Parametric diagrams and equations8.2Mass, power and data budgets8.3Integration with Simulink and Modelica8.4Co-simulation using the FMI standard8.5State machine simulation8.6Performance analysis8.7Reliability analysis from the model8.8Multidisciplinary optimisation from the model8.9Uncertainty management8.10Practical exercise: automated power budget
9.1Model-based safety assessment9.2FHA from the model9.3Fault tree generation9.4FMEA from the architecture9.5Integration with ARP4761A9.6MBSA assessment tools9.7Fault propagation analysis9.8Model-based cybersecurity9.9Validation of the safety model9.10Case study: FMEA generated from a Capella model
10.1Verification plans in the model10.2Test cases from requirements10.3Digital thread and digital twin10.4Integration with test benches10.5Model validation10.6Credibility of models and simulation10.7Evidence management10.8Formal model-based reviews10.9Certification with models10.10Workshop: verification matrix generated from the model
11.1Managing cultural change11.2Model governance11.3Configuration management of models11.4Collaboration in distributed teams11.5Integration with PLM11.6MBSE maturity metrics11.7Training engineers11.8Return on investment11.9Industrial implementation cases11.10Case study: MBSE adoption roadmap
12.1Definition of the aerospace system12.2Stakeholder and mission analysis12.3Requirements model12.4Development of the functional architecture12.5Development of the physical architecture12.6Parametric performance analysis12.7Model-based safety analysis12.8Verification plan12.9Master's Thesis report12.10Master's Thesis: defence before a panel
How you'll learn
100% online training on the SEIUM campus, with downloadable material, recorded classes and an assigned technical tutor. No fixed timetables: you progress at your own pace within the intake, so it fits alongside your job.
Each module combines theory, guided reading of the original standard and applied exercises. The working software is Cameo Systems Modeler, Capella, IBM Rhapsody, MATLAB/Simulink and Enterprise Architect, in free, academic or evaluation versions. Practice is based on real procedures for SysML modelling of aeronautical systems, parametric analysis from the model and generation of safety analyses from the architecture. Assessment is continuous by module, plus the final Master's Thesis.
Standards covered: ISO/IEC/IEEE 15288:2023, ISO/IEC/IEEE 42010, OMG SysML v1.7, OMG SysML v2, SAE ARP4754A, ECSS-E-ST-10C, ECSS-E-TM-10-25A, NASA/SP-2016-6105 Systems Engineering Handbook.
Build it end to end
Your final project follows the real engineering workflow, step by step, reviewed by your tutor.
Where this takes you
Requirements
- A university degree in engineering, science or architecture, or equivalent demonstrable professional experience.
- 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.
Frequently asked questions
The programme totals 1,900 hours over 12–14 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.
You work with Cameo Systems Modeler, Capella, IBM Rhapsody, MATLAB/Simulink and Enterprise Architect, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.
A SEIUM Institute diploma, awarded on passing the continuous assessment and the Master's Thesis. 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 in a course or postgraduate diploma in the same area are recognised in the higher programme. Ask about the recognition policy when you enrol.
A university degree in engineering, science or architecture (or equivalent professional experience), a computer able to run the programme software, and English sufficient 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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