Postgraduate DiplomaDefense, Military Engineering & Land Systems Applications open

Diploma in Tactical Aircraft Design

Online postgraduate diploma of 800 hours in tactical aircraft design: 8 modules covering conceptual design, configuration, weight and balance, performance, structures, systems and avionics, and cost and certification, with an assigned technical tutor.

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

Diploma in Tactical Aircraft Design — studying from Canada

Canada's defence sector is centred on procurement and sustainment through the Department of National Defence and Defence Research and Development Canada. Industrial activity spans land vehicles, naval systems, avionics and electronics, with firms in Ontario, Québec, Nova Scotia and British Columbia. Companies such as General Dynamics Land Systems Canada and Lockheed Martin Canada are notable employers, alongside a broad base of small and medium suppliers. Engineers work on systems integration, vehicle protection, logistics and sustainment, operating within strict security and export control frameworks.

Fees for Canada: C$2,330 (Canadian dollar), with instalments and employer sponsorship available.

Relevant bodies in Canada

  • Department of National Defence (DND)
  • Defence Research and Development Canada (DRDC)
  • Canadian Association of Defence and Security Industries (CADSI)
  • Public Services and Procurement Canada

Typical roles

  • Defence Systems Engineer
  • Land Systems Engineer
  • Systems Integration Engineer
  • Sustainment Engineer

Questions from Canada

Which Canadian bodies or processes govern defence engineering recognition?

Defence engineering in Canada often involves government procurement and security clearances, and engineers typically hold provincial Professional Engineer licences where a title is required. SEIUM's qualifications are private and not official state degrees or accredited by a national body, so they do not confer licensing or clearance. Recognition is for employers or the relevant body to decide, so verify this first.

Would Canadian defence or land systems employers accept this training?

Canadian defence employers and contractors generally rely on security clearance, licensing and demonstrated experience. A private qualification may support your application, but it is unlikely to replace those requirements, and its acceptance is up to each employer. A SEIUM final project can help show applied skill, so discuss expectations with prospective employers early.

Can I study remotely while working, and what are the costs and language demands?

Yes, the programmes are fully online, so you can study from Canada or elsewhere without a student visa, and fit sessions around work. Specialist courses are 300 hours, postgraduate diplomas 800 and master's 1,900. Teaching is in English, supported by an assigned technical tutor. Fees are payable in instalments, and employer sponsorship may be available.

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Learning outcomes

What you will be able to do

01

Apply the conceptual aircraft design methodology.

02

Define the configuration and geometry.

03

Manage weight and balance.

04

Calculate performance and manoeuvrability diagrams.

05

Establish loads and preliminary structures.

06

Define the systems architecture.

07

Estimate costs and plan certification.

Profile

Who it's for

  • Aircraft design engineers moving into military and training aircraft.
  • Performance engineers.
  • Weights engineers.
  • Structures engineers working on airframes.
  • Systems engineers in aeronautical programmes.
  • Programme cost analysts.
  • Engineering or science graduates seeking to enter the aerospace industry.
Standards & tools

What you'll work with

  • JSSG-2001B (air vehicle joint service specification guide)
  • JSSG-2006 (aircraft structures)
  • MIL-HDBK-516C (airworthiness certification criteria)
  • MIL-STD-1797A (flying qualities of piloted aircraft)
  • EMAR 21 (European military airworthiness certification requirements)
  • OpenVSP
  • XFLR5
  • MATLAB
  • CATIA V5
  • SUAVE
Syllabus

8 modules

  1. 1.1Design process according to Raymer and Roskam
  2. 1.2Mission requirements
  3. 1.3Mission profiles
  4. 1.4Initial weight estimation
  5. 1.5Fuel fractions
  6. 1.6Wing loading and thrust-to-weight ratio
  7. 1.7Constraint diagrams
  8. 1.8Alternative configurations
  9. 1.9Trade studies
  10. 1.10Practical: initial sizing of an advanced trainer
  1. 2.1Wing planform
  2. 2.2Sweep and aspect ratio
  3. 2.3Tail surfaces
  4. 2.4Canard configuration
  5. 2.5Fuselage design
  6. 2.6Air intakes
  7. 2.7Landing gear
  8. 2.8Internal volume
  9. 2.9Engine integration
  10. 2.10Workshop: configuration in OpenVSP
  1. 3.1Statistical weight methods
  2. 3.2Weight breakdown
  3. 3.3Centre of gravity
  4. 3.4Centre-of-gravity envelope
  5. 3.5Moments of inertia
  6. 3.6Weight growth
  7. 3.7Design margins
  8. 3.8Weight management
  9. 3.9Fuel burn and balance
  10. 3.10Case study: balance diagram
  1. 4.1Take-off and landing
  2. 4.2Climb
  3. 4.3Cruise
  4. 4.4Range and endurance
  5. 4.5Sustained turn
  6. 4.6Specific excess power
  7. 4.7Flight envelope
  8. 4.8Energy-manoeuvrability diagrams
  9. 4.9Agility
  10. 4.10Lab: energy-manoeuvrability diagram
  1. 5.1Design loads
  2. 5.2V-n diagram
  3. 5.3Load factors according to JSSG-2006
  4. 5.4Material selection
  5. 5.5Structural layout
  6. 5.6Fatigue
  7. 5.7Damage tolerance
  8. 5.8Structural weight estimation
  9. 5.9Composite structures
  10. 5.10Case study: V-n diagram of a trainer
  1. 6.1Fly-by-wire flight controls
  2. 6.2Hydraulic system
  3. 6.3Electrical system
  4. 6.4Fuel system
  5. 6.5Environmental control
  6. 6.6Avionics
  7. 6.7Cockpit design
  8. 6.8Crew escape systems
  9. 6.9Maintainability
  10. 6.10Practical: systems architecture
  1. 7.1DAPCA IV cost model
  2. 7.2Life-cycle cost
  3. 7.3Production
  4. 7.4EMAR military certification
  5. 7.5Development testing
  6. 7.6Sustainment
  7. 7.7Programme risks
  8. 7.8Exports
  9. 7.9M-346, T-7A and PC-21 programmes
  10. 7.10Case study: cost estimation with DAPCA
  1. 8.1Mission requirements
  2. 8.2Sizing
  3. 8.3Configuration
  4. 8.4Weight and balance
  5. 8.5Performance
  6. 8.6Preliminary structure
  7. 8.7Systems
  8. 8.8Cost and feasibility
  9. 8.9Report and presentation
  10. 8.10Final project: final review with the tutor
Methodology, software & labs

How you'll learn

A 100% online programme 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 OpenVSP, XFLR5, MATLAB, CATIA V5 and SUAVE, in free, academic or evaluation versions. Practice is based on real procedures for conceptual aircraft sizing, performance analysis and configuration trade studies. Assessment is continuous by module plus the final project.

Standards covered: JSSG-2001B, JSSG-2006, MIL-HDBK-516C, MIL-STD-1797A, EMAR 21.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of JSSG-2001B, JSSG-2006 and MIL-HDBK-516C applied to real cases, not as a theoretical annex.
Industry software:OpenVSP, XFLR5, MATLAB, CATIA V5 and SUAVE, in free, academic or evaluation versions.
Final project:A conceptual design of a tactical aircraft, from mission requirements to cost and feasibility, 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.

Define the mission
Set the mission requirements and profiles and carry out initial sizing with constraint diagrams.
Develop the configuration
Model the configuration and geometry in OpenVSP and integrate the engine.
Weight, balance and performance
Prepare the weight breakdown, balance diagram and energy-manoeuvrability analysis.
Structure, systems and cost
Define the V-n diagram, preliminary structure, systems architecture and DAPCA cost estimate.
Final project
Deliver the complete design report and presentation, reviewed by your tutor.
Career opportunities

Where this takes you

Aircraft design engineerPerformance engineerWeights engineerStructures engineerSystems engineerProgramme cost analyst
Admissions & scholarships

Requirements

  • Prior technical training or professional experience in the sector. No university degree is required.
  • 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 OpenVSP, XFLR5, MATLAB, CATIA V5 and SUAVE, 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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