CourseAerospace, UAM, Drones & Space Applications open

Propulsion-Structure Integration Course

Online course of 300 hours in propulsion-structure integration, structured in 6 modules covering aircraft engine installation, loads and design cases, mount and pylon design, dynamics and vibration, and integration in space vehicles, with an assigned technical tutor.

Duration3 months
ModeOnline
LanguageEnglish
Start datesSet by the faculty
AwardSEIUM Institute certificate

Propulsion-Structure Integration Course — studying from India

India's aerospace sector is growing steadily, anchored by Bengaluru, Hyderabad and the Kanpur-Lucknow belt. Hindustan Aeronautics Limited, Tata Advanced Systems and Bharat Electronics are major employers, alongside a fast-growing base of drone and space start-ups. The Indian Space Research Organisation and the Defence Research and Development Organisation drive research programmes, while civil aviation rules are set by the Directorate General of Civil Aviation. Engineers here work on aircraft systems, unmanned aerial vehicles, satellite subsystems and urban air mobility concepts, and the sector's push for indigenisation keeps demand for skilled talent strong.

Fees for India: ₹68,400 (Indian Rupee), with instalments and employer sponsorship available.

Relevant bodies in India

  • Directorate General of Civil Aviation (DGCA)
  • Indian Space Research Organisation (ISRO)
  • Aeronautical Society of India
  • Bureau of Indian Standards (BIS)

Typical roles

  • Aerospace Engineer
  • Avionics Engineer
  • Drone Systems Engineer
  • Satellite Systems Engineer

Questions from India

Which professional bodies in India recognise aerospace engineering, and does a private online qualification help with recognition?

In India, aeronautical engineering is recognised mainly through the Institution of Engineers (India), the Aeronautical Society of India and the Directorate General of Civil Aviation for aircraft maintenance licences. SEIUM's qualifications are private, not state degrees, and are not accredited by any national body. Whether they count towards professional membership or roles is decided by the employer or the relevant body, so check their criteria before enrolling.

Which employers in India hire aerospace engineers, and how would this programme be used in that work?

Aerospace engineers in India work with organisations such as ISRO, HAL, DRDO laboratories, and private aerospace and drone firms, along with MRO and airline engineering teams. A private postgraduate qualification can support a career move or specialisation, but it is not a substitute for formal technical experience or statutory certifications. Employers usually weigh it alongside your work record and skills.

Can I manage this programme alongside a full-time job in India, given the time zone and language?

The programme is 100% online and taught in English, so you can study from home without a student visa. Classes and deadlines are set by the school, so check the schedule against India Standard Time (IST). Master's programmes are around 1,900 hours, postgraduate diplomas around 800 and specialist courses around 300, so plan your weekly hours realistically. You get an assigned technical tutor. Ask your employer about sponsorship, as instalment fees may make this easier.

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Learning outcomes

What you will be able to do

01

Identify the load paths between the propulsion system and the structure.

02

Calculate the critical load cases for mounts and pylons.

03

Design fail-safe supports using fatigue and damage tolerance criteria.

04

Analyse coupled engine-structure dynamics.

05

Assess the integration of rocket engines and thrusters in space vehicles.

06

Apply finite element models to integration analysis.

07

Justify the structural compliance of a propulsion installation.

Profile

Who it's for

  • Aircraft structures engineers working on pylons and nacelles.
  • Propulsion integration engineers at airframe and engine manufacturers.
  • Loads analysts defining engine installation load cases.
  • Structural dynamics engineers dealing with coupled modes and flutter.
  • Structural certification engineers preparing compliance justifications.
  • Launcher design engineers working on thrust frames and stages.
  • Engineering or science graduates looking to enter aircraft manufacturing.
Standards & tools

What you'll work with

  • CS-25 (EASA certification specifications for large aeroplanes)
  • 14 CFR Part 25 (FAA airworthiness standards for transport category aeroplanes)
  • CS-E (EASA certification specifications for engines)
  • FAA AC 20-107B (composite aircraft structure)
  • MMPDS (metallic materials properties for aerospace structures)
  • CMH-17 (composite materials handbook)
  • ECSS-E-ST-32C (space engineering, structural general requirements)
  • ECSS-E-ST-32-10C (structural factors of safety for spaceflight hardware)
  • MSC Nastran
  • Abaqus
  • Altair HyperMesh
  • Ansys Mechanical
  • Femap
Syllabus

6 modules

  1. 1.1Under-wing, fuselage and tail-mounted configurations
  2. 1.2Pylons, mounts and nacelles
  3. 1.3Engine-wing load paths
  4. 1.4Thrust, torque and gyroscopic loads
  5. 1.5Certification load cases
  6. 1.6Engine-wing aerodynamic interaction
  7. 1.7Installation of propellers and turboprops
  8. 1.8Integration in launchers and satellites
  9. 1.9Load paths in the nacelle and thrust reverser
  10. 1.10Workshop: load diagram of a pylon
  1. 2.1Limit and ultimate loads
  2. 2.2Engine seizure torque
  3. 2.3Blade loss and unbalance
  4. 2.4Landing and gust loads on the engine
  5. 2.5Thermal loads from the exhaust
  6. 2.6Pressure loads in the nacelle
  7. 2.7Combination of load cases
  8. 2.8Applicable safety factors
  9. 2.9Ingestion loads and engine separation
  10. 2.10Practical: calculation of loads on engine mounts
  1. 3.1Forward and aft mounts
  2. 3.2Fail-safe design and redundant load paths
  3. 3.3Materials: titanium, Inconel and composites
  4. 3.4Fatigue and damage tolerance
  5. 3.5Critical joints and bolts
  6. 3.6Vibration isolators
  7. 3.7Firewalls and thermal protection
  8. 3.8Maintainability and access
  9. 3.9Structural fuses and controlled separation
  10. 3.10Case study: analysis of a mount with simulated failure
  1. 4.1Coupled engine-wing modes
  2. 4.2Flutter with engine masses
  3. 4.3Vibration transmission to the cabin
  4. 4.4Response to rotor unbalance
  5. 4.5Windmilling after blade loss
  6. 4.6Isolation and damping
  7. 4.7Ground vibration testing
  8. 4.8Rotor modelling in structural analysis
  9. 4.9Dynamic response to bird strikes
  10. 4.10Lab: modal analysis of an engine-pylon assembly
  1. 5.1Rocket engine thrust and stage structure
  2. 5.2Engine thrust frames and gimbal
  3. 5.3POGO oscillations
  4. 5.4Launch loads on satellite thrusters
  5. 5.5Attachment of tanks and thrusters
  6. 5.6Thermal distortion and thrust alignment
  7. 5.7Structural qualification testing
  8. 5.8Lessons from launcher integration
  9. 5.9Thruster joints in sandwich panels
  10. 5.10Case study: thrust alignment on a satellite
  1. 6.1Definition of the configuration
  2. 6.2Critical load cases
  3. 6.3Preliminary design of the support
  4. 6.4Finite element model
  5. 6.5Static and fatigue analysis
  6. 6.6Dynamic and modal analysis
  7. 6.7Compliance justification
  8. 6.8Test plan
  9. 6.9Report and presentation
  10. 6.10Final 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. There are no fixed timetables: you progress at your own pace within each intake, so the programme is compatible with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is MSC Nastran, Abaqus, Altair HyperMesh, Ansys Mechanical and Femap, in free, academic or evaluation versions. Testing is studied through real procedures: finite element modelling of an engine pylon, blade-loss load analysis, and modal study of a rocket engine thrust frame. Assessment is continuous by module, plus the final project.

Standards covered: CS-25, 14 CFR Part 25, CS-E, FAA AC 20-107B, MMPDS, CMH-17, ECSS-E-ST-32C, ECSS-E-ST-32-10C.

Assigned technical tutor:every module ends with a deliverable that your tutor marks individually.
Standards-based learning:guided reading of CS-25, 14 CFR Part 25 and CS-E applied to real cases, not as a theoretical annex.
Industry software:MSC Nastran, Abaqus, Altair HyperMesh, Ansys Mechanical and Femap, in free, academic or evaluation versions.
Final project:the structural integration of a propulsion installation, from critical load cases and preliminary support design to FE model, static, fatigue and modal analysis and compliance justification, 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.

Pylon load diagram
Draw the load diagram of an engine pylon.
Engine mount loads
Calculate the loads on the engine mounts for the critical cases.
Fail-safe mount analysis
Analyse a mount with a simulated failure of one load path.
Modal analysis
Perform the modal analysis of an engine-pylon assembly.
Final project
Justify the structural compliance of a propulsion installation, reviewed by your tutor.
Career opportunities

Where this takes you

Aircraft structures engineerPropulsion integration engineerLoads analystStructural dynamics engineerStructural certification engineerLauncher design engineer
Admissions & scholarships

Requirements

  • No prior qualification 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 300 hours over 3 months. You set your own pace within each intake, and your tutor helps you plan the workload around your job.

You work with MSC Nastran, Abaqus, Altair HyperMesh, Ansys Mechanical and Femap, using free, academic or evaluation versions. Your tutor indicates the free alternative wherever one exists.

A SEIUM Institute certificate, 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.

No prior qualification is required; you need 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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