Master'sAerospace, UAM, Drones & Space Applications open

Master’s in Space Radiation and Rad-Hard Components Engineering

Online master's programme of 1,900 hours in space radiation and rad-hard components engineering: 12 modules covering the radiation environment, radiation-matter interaction, total dose, single-event and displacement damage effects, rad-hard and COTS components, design mitigation, space FPGAs and processors, radiation testing and hardness assurance, with an assigned technical tutor.

Duration1900 h
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute diploma

Master’s in Space Radiation and Rad-Hard Components Engineering — studying from Australia

Australia's aerospace sector spans defence and commercial aviation, maintenance, repair and overhaul, and a growing space industry. Key clusters sit around Adelaide's Edinburgh Parks and the Melbourne and Sydney defence precincts, with major employers including Airbus Australia Pacific, BAE Systems Australia, Boeing Defence Australia and Lockheed Martin Australia. Recreational and commercial drone operations are increasingly regulated, and advanced air mobility is emerging as a research and policy priority. Engineers working in this area typically support airworthiness, systems integration, structures and avionics across both crewed and uncrewed platforms.

Fees for Australia: A$9,410 (AUD), with instalments and employer sponsorship available.

Relevant bodies in Australia

  • Civil Aviation Safety Authority (CASA)
  • Australian Transport Safety Bureau (ATSB)
  • Defence Science and Technology Group (DSTG)
  • Standards Australia

Typical roles

  • Aerospace Engineer
  • Avionics Engineer
  • Airworthiness Engineer
  • Drone Systems Engineer

Questions from Australia

Does a SEIUM qualification help me get recognised by a professional body in Australia?

SEIUM qualifications are private qualifications, not official state degrees, and they are not accredited by any Australian body. Engineers Australia accredits university engineering degrees, and the Civil Aviation Safety Authority (CASA) regulates drone and aviation operations. Recognition of a private qualification is decided by the employer or the relevant body, so check with them before enrolling.

Will this course help me find work in Australian aerospace, drones or space?

Australia has aerospace and defence employers, drone operators and space-sector companies, and skills in these areas are valued. Whether a SEIUM qualification counts for a given role depends on the employer, who will usually weigh your experience and portfolio alongside any private credential. Ask prospective employers how they view it.

Can I study this part-time while working, and does the time zone suit Australia?

The programmes are fully online and taught in English, so you can study from anywhere in Australia, with no student visa needed for home study. Master's programmes total 1,900 hours, postgraduate diplomas 800 hours and specialist courses 300 hours, so plan your weekly load realistically. Fees are payable in instalments, and employer sponsorship may be possible.

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Learning outcomes

What you will be able to do

01

Understand the space radiation environment.

02

Analyse the interaction of radiation with electronic components.

03

Assess total dose, single-event and displacement effects.

04

Select suitable rad-hard and COTS components.

05

Design mitigations at system and circuit level.

06

Plan radiation tests.

07

Apply radiation assurance in space projects.

Profile

Who it's for

  • Radiation effects engineers looking for a structured, standards-based framework.
  • Space EEE component engineers responsible for part selection and approval.
  • Product assurance engineers who handle radiation hardness assurance.
  • Space electronics designers who need to build in tolerance from the start.
  • Space FPGA engineers working on mitigation and testing.
  • Radiation physics researchers moving into applied space engineering.
  • Engineering or science graduates aiming to enter the space sector.
Standards & tools

What you'll work with

  • ECSS-E-ST-10-04C (space environment)
  • ECSS-E-ST-10-12C (methods for the calculation of radiation received)
  • ECSS-Q-ST-60-15C (radiation hardness assurance)
  • ESCC Basic Specification 22900 (total dose steady-state irradiation test method)
  • ESCC Basic Specification 25100 (single-event effects test method)
  • MIL-STD-883 Method 1019 (ionising radiation (total dose) test procedure)
  • ECSS-Q-ST-60C (EEE components)
  • JESD57 (heavy-ion single-event effects testing)
  • SPENVIS
  • OMERE
  • Geant4
  • FASTRAD
  • CREME96
Syllabus

12 modules · 1900 h

  1. 1.1Van Allen belts and their dynamics
  2. 1.2Galactic cosmic rays
  3. 1.3Solar particle events
  4. 1.4South Atlantic Anomaly
  5. 1.5Radiation in LEO, MEO and GEO orbits
  6. 1.6AE9/AP9 and CREME96 models
  7. 1.7LET and energy spectra
  8. 1.8Space weather and its forecasting
  9. 1.9Environments for Jupiter and deep-space missions
  10. 1.10Lab: radiation spectrum of an orbit with SPENVIS
  1. 2.1Ionisation and linear energy transfer
  2. 2.2Atomic displacement and NIEL
  3. 2.3Total ionising dose
  4. 2.4Proton and neutron interaction
  5. 2.5Secondary particles in shielding
  6. 2.6Charge physics in oxides
  7. 2.7Effects on materials and optical sensors
  8. 2.8Units and dosimetry
  9. 2.9Particle transport tools
  10. 2.10Practical exercise: dose calculation behind aluminium shielding
  1. 3.1Threshold voltage shift
  2. 3.2Leakage currents
  3. 3.3ELDRS effects in bipolar transistors
  4. 3.4Degradation in analogue components
  5. 3.5Effects on memories
  6. 3.6Annealing and dose-rate-dependent effects
  7. 3.7RDM design margins
  8. 3.8Testing to ESCC 22900
  9. 3.9Testing with cobalt-60 sources
  10. 3.10Case study: dose margin analysis of a regulator
  1. 4.1SEU and MBU in memories
  2. 4.2SET in logic and analogue devices
  3. 4.3SEL and its protection
  4. 4.4SEGR and SEB in power MOSFETs
  5. 4.5SEFI in complex devices
  6. 4.6Cross-section and Weibull curves
  7. 4.7Calculation of in-orbit error rates
  8. 4.8Heavy-ion testing
  9. 4.9Proton testing
  10. 4.10Lab: SEU rate with a Weibull curve
  1. 5.1Effects on solar cells
  2. 5.2Degradation of CCD and CMOS detectors
  3. 5.3Optocouplers and LEDs
  4. 5.4Charge transfer in sensors
  5. 5.5Displacement damage dose models
  6. 5.6Proton and neutron testing
  7. 5.7Mitigation by design
  8. 5.8Impact on observation missions
  9. 5.9Examples of in-flight degradation
  10. 5.10Practical exercise: efficiency degradation of a solar panel
  1. 6.1Rad-hard by process technologies
  2. 6.2Rad-hard by design
  3. 6.3Silicon-on-insulator technology
  4. 6.4Components from the EPPL list
  5. 6.5QML-V and QML-Q components
  6. 6.6Space component manufacturers
  7. 6.7ESCC quality classes
  8. 6.8Costs and lead times
  9. 6.9European non-ITAR components
  10. 6.10Case study: selecting a processor for a GEO mission
  1. 7.1New space and the use of COTS
  2. 7.2Risks of COTS
  3. 7.3Screening and lot acceptance
  4. 7.4Radiation testing of COTS
  5. 7.5AEC-Q100 automotive components
  6. 7.6System-level mitigation strategies
  7. 7.7Experience in CubeSats
  8. 7.8ECSS standards for COTS
  9. 7.9Risk management in constellations
  10. 7.10Workshop: COTS evaluation plan for a constellation
  1. 8.1Shielding and sector analysis
  2. 8.2Triple modular redundancy (TMR)
  3. 8.3EDAC error detection and correction codes
  4. 8.4Memory scrubbing
  5. 8.5Watchdogs and supervision
  6. 8.6Latch-up protection
  7. 8.7Design of tolerant FPGAs
  8. 8.8Fault-tolerant architectures
  9. 8.9Fault-tolerant software
  10. 8.10Lab: implementing EDAC in memory
  1. 9.1Antifuse and flash FPGAs
  2. 9.2Tolerant SRAM FPGAs
  3. 9.3European NanoXplore BRAVE FPGAs
  4. 9.4LEON and GR740 processors
  5. 9.5Space ARM processors
  6. 9.6Mitigation in SRAM FPGAs
  7. 9.7Design tools
  8. 9.8Radiation testing of FPGAs
  9. 9.9Trends in space computing
  10. 9.10Practical exercise: sensitivity analysis of an FPGA design
  1. 10.1European test facilities
  2. 10.2Campaign planning
  3. 10.3Device preparation
  4. 10.4Real-time measurements
  5. 10.5Data analysis
  6. 10.6ESCC 25100 and MIL-STD-883 standards
  7. 10.7Low-dose-rate testing
  8. 10.8Pulsed laser testing
  9. 10.9Test reports
  10. 10.10Case study: heavy-ion test plan
  1. 11.1Requirements of ECSS-Q-ST-60-15C
  2. 11.2Radiation hardness assurance
  3. 11.3Worst-case analysis
  4. 11.4Radiation databases
  5. 11.5Management of critical components
  6. 11.6Design review
  7. 11.7Requirements verification
  8. 11.8Lessons from in-flight anomalies
  9. 11.9Radiation documentation
  10. 11.10Practical exercise: RHA analysis of an electronic board
  1. 12.1Mission and orbit definition
  2. 12.2Radiation environment analysis
  3. 12.3Component selection
  4. 12.4Dose and shielding analysis
  5. 12.5Calculation of single-event rates
  6. 12.6Mitigation design
  7. 12.7Test plan
  8. 12.8Radiation assurance analysis
  9. 12.9Master's Thesis: written report
  10. 12.10Master's Thesis: defence before a panel
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 each intake, so it fits around your job.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is SPENVIS, OMERE, Geant4, FASTRAD and CREME96, in free, academic or evaluation versions. Testing is studied through real procedures for total dose testing with cobalt-60, single-event testing with heavy ions and sector shielding analysis. Assessment is continuous by module, plus the final Master's Thesis.

Standards covered: ECSS-E-ST-10-04C, ECSS-E-ST-10-12C, ECSS-Q-ST-60-15C, ESCC Basic Specification 22900, ESCC Basic Specification 25100, MIL-STD-883 Method 1019, ECSS-Q-ST-60C, JESD57.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of ECSS-E-ST-10-04C, ECSS-E-ST-10-12C and ECSS-Q-ST-60-15C applied to real cases, not as a theoretical annex.
Industry software:SPENVIS, OMERE, Geant4, FASTRAD and CREME96, in free, academic or evaluation versions.
Master's Thesis with defence:A complete radiation hardness assurance analysis for a space mission, from environment and component selection to mitigation and test plan, defended before a panel.
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.

Mission and environment
Define the mission and orbit and analyse its radiation environment.
Components and shielding
Select the components and analyse dose and shielding.
Single-event rates and mitigation
Calculate single-event rates and design the mitigations.
Test plan and RHA
Draft the radiation test plan and the radiation assurance analysis.
Master's Thesis
Present the integrated radiation hardness assurance study, defended before a panel.
Career opportunities

Where this takes you

Radiation effects engineerSpace EEE component engineerProduct assurance engineerSpace electronics designerSpace FPGA engineerRadiation physics researcher
Admissions & scholarships

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.

FAQ

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 SPENVIS, OMERE, Geant4, FASTRAD and CREME96, 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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