EN 14607-2:2004

Foreword
1 Scope
2 Normative references
3 Terms, definitions, abbreviated terms and units
  3.1 Terms and definitions
  3.2 Abbreviated terms
4 Requirements
  4.1 General
  4.2 Mission
       4.2.1 Lifetime
       4.2.2 Natural and induced environment
       4.2.3 Mechanical environment
       4.2.4 Microgravity, audible noise and human vibration
       4.2.5 Corrosion effects
       4.2.6 Ablation and pyrolysis
       4.2.7 Micrometeoroid and debris collision
       4.2.8 Venting and purging
       4.2.9 Mass and inertia properties
       4.2.10 Load events
       4.2.11 Limit loads
       4.2.12 Design loads
       4.2.13 Structural reliability
  4.3 Functionality
       4.3.1 Strength
       4.3.2 Buckling
       4.3.3 Stiffness
       4.3.4 Dynamic behaviour
       4.3.5 Thermal
       4.3.6 Pressure
       4.3.7 Damage tolerance
       4.3.8 Fracture control
       4.3.9 Tolerances and alignments
       4.3.10 Electrical conductivity
       4.3.11 Lightning protection
       4.3.12 Electromagnetic compatibility
       4.3.13 Dimensional stability
  4.4 Constraints
  4.5 Interface
  4.6 Design
       4.6.1 Inspectability
       4.6.2 Interchangeability
       4.6.3 Maintainability
       4.6.4 Availability
       4.6.5 Design concept
       4.6.6 Design optimization
       4.6.7 Material allowables
       4.6.8 Metals
       4.6.9 Non-metallic materials
       4.6.10 Composite fibre reinforced materials
       4.6.11 Adhesive materials in bonded joints
       4.6.12 Margin of safety (MOS)
       4.6.13 Factors of safety (FOS)
       4.6.14 Scatter factors
  4.7 Verification
       4.7.1 General verification
       4.7.2 Verification by analysis
       4.7.3 Modelling aspects
       4.7.4 Static analysis
       4.7.5 Modal analysis
       4.7.6 Response analysis
       4.7.7 Acoustics analysis
       4.7.8 Fluid structure interaction (FSI)
       4.7.9 Fatigue analysis
       4.7.10 Fracture mechanics analysis
       4.7.11 Verification of composite structures
       4.7.12 Buckling analysis
       4.7.13 Thermo-elastic analysis
       4.7.14 Adhesive connections
       4.7.15 Bolted connections
       4.7.16 Welded connections
       4.7.17 Riveted connections
       4.7.18 Insert connections
       4.7.19 Aeroelasticity
       4.7.20 Mass and inertia properties
       4.7.21 Alignments
       4.7.22 Dimensional stability
       4.7.23 Microgravity, audible noise and human vibration
              analysis
       4.7.24 Verification by test
       4.7.25 Static test
       4.7.26 Modal survey test
       4.7.27 Dynamic tests: sine, random, shock
       4.7.28 Acoustic test
       4.7.29 Fatigue and fracture test
       4.7.30 Microgravity, audible noise and human vibration
              tests
       4.7.31 Non-destructive inspection and test
       4.7.32 Thermal stress and distortion test
       4.7.33 Thermal cycling test
       4.7.34 Ageing test
       4.7.35 Contamination test
       4.7.36 Mass and Inertia properties measurement
       4.7.37 Alignment checks
       4.7.38 Dimensional stability tests
       4.7.39 Geometrical control
       4.7.40 Interface verification
       4.7.41 Aerothermodynamic test
       4.7.42 Aeroelasticity test
       4.7.43 Lightning protection verification
  4.8 Production and manufacturing
       4.8.1 General
       4.8.2 Procurement
       4.8.3 Manufacturing process
       4.8.4 Manufacturing drawings
       4.8.5 Tooling
       4.8.6 Component manufacture
       4.8.7 Assembly
       4.8.8 Storage
       4.8.9 Cleanliness
       4.8.10 Health and safety
  4.9 In-service
       4.9.1 Ground inspection
       4.9.2 In-orbit inspection
       4.9.3 Evaluation of damage
       4.9.4 Maintenance
       4.9.5 Repair
  4.10 Data exchange
       4.10.1 General
       4.10.2 System and structure subsystem
       4.10.3 Design and manufacturing
       4.10.4 Design and structural analysis
       4.10.5 Other subsystem and structural analysis
       4.10.6 Tests and structural analysis
       4.10.7 Structural mathematical models
  4.11 Product assurance
       4.11.1 General
       4.11.2 Model traceability
  4.12 Deliverables
       4.12.1 General
       4.12.2 Documents
Annex A (informative) Effective mass definition
Annex B (informative) Spacecraft (STM approach)
        development assumptions
      B.1 Development assumptions
      B.2 Loads and factors relationship
      B.3 Common factors values
Annex C (informative) Launcher structural element
      C.1 Development assumptions
      C.2 Loads and factors relationships
      C.3 Common factors values for ARIANE