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CourseDefense, Military Engineering & Land Systems Applications open

NATO Standardisation Course in helicopter crashworthiness

Online 300-hour course in NATO standardisation in helicopter crashworthiness. 6 modules covering MIL-STD-1290A (impact resistance of rotary-wing aircraft), CS-29.561 and CS-29.562 (emergency landing conditions) and LS-DYNA. Assigned tutor and open enrolment.

Duration300 h
ModeOnline
Start datesSet by the faculty
AwardSEIUM Institute certificate
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Learning outcomes

What you will be able to do

01

Explain the principles of impact survivability in helicopters.

02

Describe the civil and military impact resistance regulatory framework.

03

Design energy-absorbing structures and landing gear.

04

Specify seats and occupant restraint systems.

05

Apply requirements for impact-resistant fuel systems.

06

Simulate an impact scenario using explicit methods.

07

Develop an impact-resistant design project.

Profile

Who it's for

  • Impact resistance engineer seeking to specialise in NATO Standardisation in helicopter crashworthiness.
  • Helicopter structures engineer seeking to specialise in NATO Standardisation in helicopter crashworthiness.
  • Explicit simulation engineer seeking to specialise in NATO Standardisation in helicopter crashworthiness.
  • Restraint systems engineer seeking to specialise in NATO Standardisation in helicopter crashworthiness.
  • Rotary-wing aircraft certification engineer seeking to specialise in NATO Standardisation in helicopter crashworthiness.
  • Dynamic test technician seeking to specialise in NATO Standardisation in helicopter crashworthiness.
  • Engineering or science graduates seeking to enter the aerospace industry.
Standards & tools

What you'll work with

  • MIL-STD-1290A (impact resistance of rotary-wing aircraft)
  • CS-29.561 and CS-29.562 (emergency landing conditions)
  • 14 CFR 29.952 (fuel system impact resistance)
  • MIL-DTL-27422 (impact-resistant fuel tanks)
  • SAE AS8049 (aircraft seats)
  • MIL-S-58095 (impact-resistant crew seats)
  • Aircraft Crash Survival Design Guide (USAAVSCOM TR 89-D-22)
Syllabus

6 modules · 300 h

  1. 1.1Helicopter accidents and survivability
  2. 1.2The concept of crashworthiness and its evolution
  3. 1.3Impact pulses and the shock environment
  4. 1.4Human tolerance to acceleration
  5. 1.5Eiband diagrams and injury criteria
  6. 1.6Habitable volume and occupant protection
  7. 1.7Chained energy absorption: landing gear, structure and seat
  8. 1.8History of the Aircraft Crash Survival Design Guide
  9. 1.9Lessons from documented military accidents
  10. 1.10Case study: analysis of an accident report
  1. 2.1MIL-STD-1290A impact resistance
  2. 2.2NATO STANAGs and AEPs on crashworthiness
  3. 2.3Relationship with EASA CS-27 and CS-29
  4. 2.4FAR 27.562 and 29.562 requirements
  5. 2.5The NATO standardisation process
  6. 2.6Organisation and committees of the NSO
  7. 2.7NH90 and Tigre programme requirements
  8. 2.8Military versus civil certification
  9. 2.9Harmonisation between nations
  10. 2.10Workshop: comparison of MIL-STD-1290A and CS-29 requirements
  1. 3.1Energy absorption in the landing gear
  2. 3.2Oleo-pneumatic dampers and collapsible elements
  3. 3.3Absorbent ground and subfloor structure
  4. 3.4Composite materials and crash behaviour
  5. 3.5Retention of heavy masses: rotor and transmission
  6. 3.6Water impact and ditching
  7. 3.7Controlled deformation zones
  8. 3.8Fuel tank integrity
  9. 3.9Crash-resistant fuel systems
  10. 3.10Practice: energy balance of a vertical impact
  1. 4.1Energy-absorbing seats
  2. 4.2Load limiters and available stroke
  3. 4.3Harnesses and restraint systems
  4. 4.4Spinal injuries and the DRI criterion
  5. 4.5Airbags in helicopter cabins
  6. 4.6Head protection and impacts against structure
  7. 4.7Occupants with equipment and anthropometric variability
  8. 4.8Dynamic seat testing
  9. 4.9Anthropomorphic dummies and FAA Hybrid III
  10. 4.10Laboratory: interpretation of a dynamic seat test
  1. 5.1Explicit impact simulation with finite elements
  2. 5.2Material and failure models
  3. 5.3Model validation through testing
  4. 5.4Full fuselage drop tests
  5. 5.5Component and substructure testing
  6. 5.6Instrumentation and data acquisition
  7. 5.7Certification by analysis supported by testing
  8. 5.8Post-crash evacuation and survival
  9. 5.9Post-impact fire resistance
  10. 5.10Case study: test–simulation correlation
  1. 6.1Definition of the aircraft and its mission
  2. 6.2Selection of applicable requirements
  3. 6.3Design impact scenarios
  4. 6.4Energy absorption strategy
  5. 6.5Seat and restraint design
  6. 6.6Design impact simulation
  7. 6.7Validation test plan
  8. 6.8Regulatory compliance matrix
  9. 6.9Report and presentation
  10. 6.10Final review with the tutor
Methodology, software & labs

How you'll learn

Training 100 % online on the SEIUM campus, with downloadable material, recorded classes and assigned technical tutor. No fixed timetables: students progress at their own pace within the intake, which makes it possible to combine with work.

Each module combines theory, guided reading of the original standard and applied exercises. The working software is LS-DYNA, Abaqus/Explicit, MADYMO, HyperMesh, in free, academic or evaluation versions. Tests are studied using real dynamic sled seat test procedures, fuselage impact simulation and fuel tank drop tests. Assessment is continuous per module plus the final integrative project.

Accredited laboratories(EN ISO/IEC 17025) with a rotor test rig, EMC/Lightning pre-compliance, HIL/SIL, vibration/acoustics.
Evidence-oriented Master's Thesis:safety case, test plan, compliance dossier and operational limits.
Industry-mentored:lecturers with experience in training, , eVTOL/UAM and flight test.
Flexible format(hybrid/online), international cohorts and support from SEIUM Career Services.
Ethics and safety:safety-by-design approach, OT cyber, DIH and compliance as core pillars.
Capstone project

Build it end to end

Your final project follows the real engineering workflow, step by step, reviewed by your tutor.

Definition of the aircraft and its mission

Explain the principles of impact survivability in helicopters.

Selection of applicable requirements

Describe the civil and military impact resistance regulatory framework.

Design impact scenarios

Design energy-absorbing structures and landing gear.

Energy absorption strategy

Specify seats and occupant restraint systems.

Seat and restraint design

Apply requirements for impact-resistant fuel systems.

Career opportunities

Where this takes you

Impact resistance engineerHelicopter structures engineerExplicit simulation engineerRestraint systems engineerRotary-wing aircraft certification engineerDynamic test technician
Admissions & scholarships

Requirements

  • No prior degree required.
  • Internet connection and a computer capable of running the programme's software.
  • Sufficient level of Spanish to follow technical regulatory reading.

Ready to start?

Send your application today. Our admissions team replies within 72 hours with your study plan and funding options.

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FAQ

Frequently asked questions

The programme comprises 300 hours in total, spread over 3 to 5 months. That is an average of 10 to 15 hours per week, compatible with a full-time job.

The course uses LS-DYNA, Abaqus/Explicit, MADYMO, HyperMesh. Free, academic or evaluation versions are used, and the tutor indicates the free alternative where one exists.

A SEIUM own diploma upon passing the continuous assessment and the integrative project. It is in-house training, not an official Ministry qualification.

Yes. Modules passed in a course or postgraduate diploma in the same area are recognised in the advanced programme. Check the recognition policy when enrolling.

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