Postgraduate DiplomaDefense, Military Engineering & Land Systems Applications open

Diploma in Structural Materials for Combat Aviation

Online postgraduate diploma of 800 hours in structural materials for combat aviation: 8 modules covering structural requirements, aluminium alloys, titanium, steels and superalloys, polymer-matrix composites, fatigue and damage tolerance, testing and advanced materials, under MMPDS, CMH-17 and MIL-STD-1530D, with an assigned technical tutor.

Duration6–8 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute diploma

Diploma in Structural Materials for Combat Aviation — studying from South Africa

South Africa has a established defence industry centred on companies such as Denel and Paramount Group, with capabilities in land systems, armoured vehicles and munitions. The sector supports engineering roles in systems integration, vehicle design and test and evaluation. Defence procurement and export controls are overseen by government bodies, and the industry works closely with the South African National Defence Force. Engineers in this field typically combine mechanical, electrical and systems skills.

Fees for South Africa: R 33 400 (South African rand), with instalments and employer sponsorship available.

Relevant bodies in South Africa

  • Department of Defence (South Africa)
  • National Conventional Arms Control Committee (NCACC)
  • South African Bureau of Standards (SABS)

Typical roles

  • Defence Systems Engineer
  • Land Systems Engineer
  • Systems Integration Engineer
  • Test and Evaluation Engineer

Questions from South Africa

Which South African bodies regulate or recognise defence and military engineering professionals?

Engineers in South Africa are registered through ECSA under the Engineering Profession Act, and defence programmes are guided by institutions such as the South African National Defence Force and Armscor, which set their own requirements. SEIUM is a private online institute, and its qualifications are not state degrees or accredited by a national body. Recognition is decided by these bodies and your employer, so confirm with them first.

Would this qualification help me find work in South Africa's defence or land systems sector?

South Africa has a defence industry with state-linked entities and private contractors, and employers usually require security clearances, relevant experience and recognised qualifications. A private online programme may support your application but does not guarantee employment or clearance. Check requirements with prospective employers, as roles in this sector can be sensitive and tightly controlled.

Can I study alongside a job, and are there funding options?

The course is 100% online and taught in English, so you need strong English, and no student visa is needed to study from home. Master's programmes are 1,900 hours, postgraduate diplomas 800 hours and specialist courses 300 hours, each with an assigned technical tutor. Fees are payable in instalments, and employer sponsorship is possible, so ask whether your employer would fund part of the training.

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Learning outcomes

What you will be able to do

01

Define the structural requirements of highly manoeuvrable aircraft.

02

Select metallic alloys according to the loads involved.

03

Design composite laminates.

04

Apply fracture mechanics and damage tolerance.

05

Plan characterisation tests according to the test pyramid.

06

Evaluate advanced materials and their sustainability.

07

Develop a complete structural component.

Profile

Who it's for

  • Aeronautical materials engineers.
  • Structural engineers.
  • Composites specialists.
  • Non-destructive testing engineers.
  • Damage tolerance engineers.
  • Aeronautical manufacturing engineers.
  • Engineering or science graduates aiming to move into the aeronautical sector.
Standards & tools

What you'll work with

  • MMPDS (Metallic Materials Properties Development and Standardization)
  • CMH-17 (Composite Materials Handbook)
  • MIL-STD-1530D (Aircraft Structural Integrity Program)
  • ASTM D3039 (tensile properties of polymer-matrix composites)
  • ASTM E647 (fatigue crack growth rates)
  • ASTM D7136 (drop-weight impact damage resistance of composites)
  • MIL-HDBK-6870 (non-destructive inspection programme requirements for aircraft)
  • Abaqus
  • Ansys Granta Selector
  • NASGRO
  • ANSYS Composite PrepPost
  • MATLAB
Syllabus

8 modules

  1. 1.1Loads on highly manoeuvrable aircraft
  2. 1.2Load factors and flight envelope
  3. 1.3Stiffness versus weight
  4. 1.4Damage tolerance
  5. 1.5Thermal environments
  6. 1.6Influence of radar signature on materials
  7. 1.7Material selection criteria
  8. 1.8Ashby charts
  9. 1.9Cost and availability
  10. 1.10Case study: material selection for a spar
  1. 2.12xxx and 7xxx series
  2. 2.2Aluminium-lithium alloys
  3. 2.3Heat treatments and tempers
  4. 2.4Corrosion and surface protection
  5. 2.5Fatigue behaviour
  6. 2.6Forming and machining
  7. 2.7Riveted joints and friction stir welding
  8. 2.8Fuselage applications
  9. 2.9MMPDS design data
  10. 2.10Laboratory: tensile testing of specimens
  1. 3.1Ti-6Al-4V alloy
  2. 3.2Titanium microstructures
  3. 3.3Forging and superplastic forming
  4. 3.4Additive manufacturing of titanium
  5. 3.5Nickel superalloys
  6. 3.6Ultra-high-strength steels
  7. 3.7Hydrogen embrittlement
  8. 3.8Materials for hot zones
  9. 3.9Life-cycle cost
  10. 3.10Practical exercise: metallographic analysis of titanium
  1. 4.1High-modulus carbon fibres
  2. 4.2Epoxy and bismaleimide resins
  3. 4.3PEEK and PEKK thermoplastics
  4. 4.4Laminates and stacking sequences
  5. 4.5Autoclave and out-of-autoclave curing
  6. 4.6Resin transfer moulding
  7. 4.7Manufacturing defects
  8. 4.8Classical laminate theory
  9. 4.9Laminate failure criteria
  10. 4.10Workshop: designing a laminate
  1. 5.1S-N curves
  2. 5.2Fracture mechanics
  3. 5.3Crack growth
  4. 5.4ASIP programme according to MIL-STD-1530
  5. 5.5Load spectra
  6. 5.6Inspection intervals
  7. 5.7Impact damage in composites
  8. 5.8Structural repairs
  9. 5.9Fleet life extension
  10. 5.10Case study: crack growth with NASGRO
  1. 6.1ASTM test standards
  2. 6.2The test pyramid
  3. 6.3Building-block approach
  4. 6.4CMH-17 data
  5. 6.5A- and B-basis allowables
  6. 6.6Hot/wet environment testing
  7. 6.7Ultrasonic inspection
  8. 6.8Thermography and radiography
  9. 6.9Materials certification
  10. 6.10Practical exercise: ultrasonic inspection of a panel
  1. 7.1Ceramics and ceramic-matrix composites
  2. 7.2Nanomaterials in structures
  3. 7.3Multifunctional materials
  4. 7.4Smart structures
  5. 7.5Structural health monitoring
  6. 7.6Composite recycling
  7. 7.7Critical raw materials
  8. 7.8Structural additive manufacturing
  9. 7.9Trends in new platforms
  10. 7.10Laboratory: SHM with strain gauges and optical fibre
  1. 8.1Component definition
  2. 8.2Load and environmental requirements
  3. 8.3Material preselection
  4. 8.4Component design
  5. 8.5Fatigue and damage analysis
  6. 8.6Test plan
  7. 8.7Manufacturing process
  8. 8.8Conclusions
  9. 8.9Report and presentation
  10. 8.10Final 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. No fixed timetables: you progress at your own pace within each intake, so you can combine it with your job.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is Abaqus, Ansys Granta Selector, NASGRO, ANSYS Composite PrepPost and MATLAB, in free, academic or evaluation versions. Practical work is based on real procedures for tensile and fatigue testing of specimens, non-destructive inspection of composite panels and crack growth analysis. Assessment is continuous by module, plus the final project.

Standards covered: MMPDS, CMH-17, MIL-STD-1530D, ASTM D3039, ASTM E647, ASTM D7136, MIL-HDBK-6870.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of MMPDS, CMH-17 and MIL-STD-1530D applied to real cases, not as a theoretical annex.
Industry software:Abaqus, Ansys Granta Selector, NASGRO, ANSYS Composite PrepPost and MATLAB, in free, academic or evaluation versions.
Final project:The complete design of a structural component, from material selection to fatigue analysis, test plan and manufacturing process, 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.

Component requirements
Define the component and its load and environmental requirements.
Material preselection
Shortlist candidate materials using Ashby charts and MMPDS/CMH-17 data.
Component design
Design the component, including the laminate where composites are used.
Fatigue and test plan
Analyse fatigue and damage tolerance and plan the characterisation tests.
Final project
A complete structural component with its manufacturing process, reviewed by your tutor.
Career opportunities

Where this takes you

Aeronautical materials engineerStructural engineerComposites specialistNon-destructive testing engineerDamage tolerance engineerAeronautical manufacturing engineer
Admissions & scholarships

Requirements

  • Prior technical training or professional experience in the sector. No university degree 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 800 hours over 6–8 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with Abaqus, Ansys Granta Selector, NASGRO, ANSYS Composite PrepPost and MATLAB, 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 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.

Prior technical training or professional experience in the sector (no university degree required), a computer able to run the 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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