Postgraduate DiplomaDefense, Military Engineering & Land Systems Applications open

Diploma in Aerothermodynamics of Combat Engines

Online postgraduate diploma of 800 hours in aerothermodynamics of combat engines. 8 modules covering military turbofan thermodynamics, supersonic intakes, fan and compressor aerodynamics, combustors and afterburners, high-temperature turbines, nozzles and integrated performance, and engine testing and certification (JSSG-2007B, MIL-HDBK-1783B, EMAR 21), with an assigned technical tutor.

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

Diploma in Aerothermodynamics of Combat Engines — studying from Malta

Malta's defence sector is comparatively small, reflecting the country's neutrality and modest armed forces. Activity centres on the Armed Forces of Malta, maritime surveillance, border security and the associated technical support. Engineering roles are mostly found in equipment maintenance, communications, infrastructure and government procurement rather than large-scale defence manufacturing. Professionals may find opportunities through public service and contractors supplying the armed forces and related agencies, where reliability and compliance with national procurement rules are important.

Fees for Malta: €895 (Euro), with instalments and employer sponsorship available.

Relevant bodies in Malta

  • Armed Forces of Malta
  • Ministry for Home Affairs, National Security and Law Enforcement
  • Department of Contracts (Malta)
  • Malta Standards Authority (MSA)

Typical roles

  • Military Systems Engineer
  • Defence Equipment Maintenance Engineer
  • Procurement Engineer
  • Communications Systems Engineer

Questions from Malta

Which bodies regulate defence and military engineering work in Malta?

Malta's Armed Forces and the Ministry responsible for defence oversee military engineering and procurement. General engineering practice is regulated by the Chamber of Engineers (KSU) under the Engineering Profession Act. Export and dual-use controls follow EU and national rules. A SEIUM qualification is private and not accredited, so any recognition depends on employers or the relevant authority.

What career paths exist in Malta for land systems and defence engineering?

Opportunities in Malta are limited and mostly within government, the Armed Forces and their suppliers, with more substantial defence industry work typically found abroad. Many roles require security clearance and specific experience. A private qualification can support your profile, but you should expect employers to focus on experience and clearance eligibility.

How do I study this from Malta, and what should I consider about workload and funding?

The programme is delivered fully online in English, with an assigned technical tutor and a final project. You do not need a visa to study from home in Malta. Durations range from 300 to 1,900 hours, so plan time alongside any work commitments. Ask about instalment payments and whether employer sponsorship is available.

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Learning outcomes

What you will be able to do

01

Analyse the thermodynamic cycle of low-bypass afterburning turbofans.

02

Design supersonic air intakes compatible with the engine.

03

Interpret compressor maps and stability margins.

04

Understand how combustors, afterburners and variable nozzles work.

05

Assess cooling solutions and materials for high-temperature turbines.

06

Simulate on- and off-design performance with professional tools.

07

Know the testing and certification requirements for military engines.

Profile

Who it's for

  • Aircraft propulsion engineers working on combat engine programmes.
  • Turbomachinery aerodynamics specialists designing fans, compressors and turbines.
  • Engine performance engineers running cycle and off-design simulations.
  • Engine test engineers in sea-level and altitude test facilities.
  • Turbomachinery CFD analysts.
  • Engine–aircraft integration engineers dealing with intakes, nozzles and installation effects.
  • Engineering or science graduates seeking to enter the aerospace industry.
Standards & tools

What you'll work with

  • JSSG-2007B (US joint service specification guide for aircraft turbine engines)
  • MIL-HDBK-1783B (Engine Structural Integrity Program, ENSIP)
  • EMAR 21 (European military airworthiness certification requirements)
  • SAE ARP755 (gas turbine engine performance station identification and nomenclature)
  • SAE ARP1420 (gas turbine engine inlet flow distortion guidelines)
  • SAE AIR1419 (inlet total-pressure distortion considerations)
  • SAE AS681 (gas turbine engine steady-state and transient performance presentation)
  • GasTurb
  • NPSS
  • ANSYS CFX
  • Simcenter STAR-CCM+
  • MATLAB
Syllabus

8 modules

  1. 1.1Ideal and real Brayton cycle
  2. 1.2Thermal, propulsive and overall efficiency
  3. 1.3Low-bypass turbofan
  4. 1.4Specific thrust and specific fuel consumption
  5. 1.5Afterburning cycle
  6. 1.6Pressure ratio and turbine entry temperature
  7. 1.7SAE ARP755 station nomenclature
  8. 1.8ISA atmosphere and altitude effects
  9. 1.9Design-point analysis
  10. 1.10Practical exercise: cycle calculation for a mixed-flow turbofan
  1. 2.1Normal and oblique shock waves
  2. 2.2Pitot, ramp and cone intakes
  3. 2.3Total pressure recovery
  4. 2.4Flow distortion and DC60 indices
  5. 2.5Intake–engine compatibility
  6. 2.6S-ducts and fan shielding
  7. 2.7Boundary layer and diverters
  8. 2.8Wind tunnel testing of intakes
  9. 2.9Distortion under SAE ARP1420
  10. 2.10Case study: preliminary design of a ramp intake
  1. 3.1Velocity triangles and the Euler equation
  2. 3.2Transonic fan and blade shocks
  3. 3.3Multistage axial compressor
  4. 3.4Compressor maps and operating line
  5. 3.5Rotating stall and surge
  6. 3.6Stability margin
  7. 3.7Variable stator vanes
  8. 3.8Bleeds and power extraction
  9. 3.9CFD of blade cascades
  10. 3.10Lab: interpretation of a fan map
  1. 4.1Annular combustors and flame stabilisation
  2. 4.2Fuel atomisation and injection
  3. 4.3NOx and soot formation
  4. 4.4Outlet temperature pattern factor
  5. 4.5Afterburner flameholders and spray rings
  6. 4.6Thermoacoustic instabilities
  7. 4.7Variable convergent–divergent nozzles
  8. 4.8Ignition and altitude relight
  9. 4.9JP-8 and F-34 fuels
  10. 4.10Workshop: energy balance of an afterburner
  1. 5.1High- and low-pressure turbines
  2. 5.2Film cooling and internal convection
  3. 5.3Thermal barrier coatings
  4. 5.4Single-crystal superalloys
  5. 5.5Profile and secondary losses
  6. 5.6Tip clearance and active control
  7. 5.7Unsteady rotor–stator interaction
  8. 5.8Creep life and thermomechanical fatigue
  9. 5.9Conjugate CFD of cooled blades
  10. 5.10Practical exercise: estimating cooling effectiveness
  1. 6.1Axisymmetric and two-dimensional nozzles
  2. 6.2Thrust vectoring
  3. 6.3Jet–airframe interaction
  4. 6.4Infrared signature of the jet and its attenuation
  5. 6.5Off-design performance
  6. 6.6Simulation with GasTurb and NPSS
  7. 6.7Acceleration and deceleration transients
  8. 6.8FADEC control and control laws
  9. 6.9Component matching
  10. 6.10Case study: performance across the flight envelope
  1. 7.1Sea-level test cells
  2. 7.2Altitude test facility testing
  3. 7.3Pressure and temperature instrumentation
  4. 7.4Bird, ice and foreign object ingestion
  5. 7.5JSSG-2007 guide requirements
  6. 7.6Structural integrity under MIL-HDBK-1783
  7. 7.7Military type certification EMAR 21
  8. 7.8Accelerated durability testing
  9. 7.9Uncertainty analysis in performance
  10. 7.10Practical exercise: data reduction from a test cell run
  1. 8.1Mission specification and requirements
  2. 8.2Selection of cycle parameters
  3. 8.3Component sizing
  4. 8.4Intake and nozzle study
  5. 8.5Off-design performance analysis
  6. 8.6Weight and fuel consumption estimate
  7. 8.7Development test plan
  8. 8.8Technical risk analysis
  9. 8.9Report and presentation
  10. 8.10Final project: final review with the tutor
Methodology, software & labs

How you'll learn

The programme is delivered 100% online 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 you can combine it with your job.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is GasTurb, NPSS, ANSYS CFX, Simcenter STAR-CCM+ and MATLAB, in free, academic or evaluation versions. Testing is studied through real procedures for sea-level engine test cell runs, intake distortion testing in wind tunnels and altitude test facility runs. Assessment is continuous by module, plus the final project.

Standards covered: JSSG-2007B, MIL-HDBK-1783B, EMAR 21, SAE ARP755, SAE ARP1420, SAE AIR1419, SAE AS681.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of JSSG-2007B, MIL-HDBK-1783B and EMAR 21 applied to real cases, not as a theoretical annex.
Industry software:GasTurb, NPSS, ANSYS CFX, Simcenter STAR-CCM+ and MATLAB, in free, academic or evaluation versions.
Final project:A combat engine project covering mission requirements, cycle selection, component sizing, intake and nozzle study, off-design performance, development test plan and technical risk 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.

Mission and cycle
Specify the mission requirements and select the engine cycle parameters.
Component sizing
Size the fan, compressor, combustor, turbines and afterburner.
Intake and nozzle
Study the supersonic intake and the variable nozzle for the design.
Off-design performance
Analyse performance across the flight envelope with GasTurb or NPSS.
Final project
Develop a complete combat engine project with development test plan and technical risk analysis.
Career opportunities

Where this takes you

Aircraft propulsion engineerTurbomachinery aerodynamics specialistEngine performance engineerEngine test engineerTurbomachinery CFD analystEngine–aircraft integration engineer
Admissions & scholarships

Requirements

  • Prior technical training or professional experience in the sector. No university degree is required.
  • An internet connection and a computer able to run the programme's 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 GasTurb, NPSS, ANSYS CFX, Simcenter STAR-CCM+ 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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