![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) |
| ![](../../global_imgs/spacer.gif) | | ![](../../global_imgs/spacer.gif) | |
![](../../global_imgs/spacer.gif) |
About us Spacecraft structuresTerms of ReferenceDuties of the Structures sectionTechnology areas Antenna structuresComposite Materials structuresFracture control / Damage toleranceInflatable structures for space applicationsMeteoroid and debris shieldingStructural verification of payloads and system hardware for human rated vehiclesStructural design and analysis Configuration studiesStructural AnalysisLauncher-Spacecraft Coupled Loads AnalysisFluid Structure InteractionVibro-Accoustic AnalysisProject support Project support activitiesServices EventsContact us
| ![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) | ![](../../global_imgs/spacer.gif) | | | ![](../../global_imgs/spacer.gif) | Composite design and analysis tools | | Composite Materials structuresComposite design and analysis tools
The Structure section has been active in supporting the development and enhancement of the ESAComp composite analysis and design program. ESAComp is nowadays widely used in European space industry for composite laminate analysis and preliminary design. Initially ESAComp was developed by the Helsinki University of Technology and now is marketed and further developed by Componeering, Finland. ESAComp has a vast set of analysis and design capabilities including the following:
- Fiber/matrix micromechanics
- Analyses for constitutive and thermal/moisture expansion behavior of plies
- Laminates
- 2.5D behavior - classical lamination theory (CLT)
- parameterized "theta-laminates" and "p-laminates"
- load response failure and design envelopes
- probabilistic 2.5D behavior
- sensitivity studies for 2.5D behavior and FPF
- notched laminate analysis of circular and elliptic holes
- Panels
- flat and curved panels with or without stiffeners
- Mindlin plate analysis using integrated Elmer FE solver
- rectangular plates
- load response, failure and stability under applied loads
- natural frequencies
- Beams and columns
- Bonded joints
- Mechanical joints
- single and double lap joints under axial loads
- fastener and by-pass loads, laminate stresses and strains on fastener holes, margins of safety for failure, prediction of failure mode
Last update: 7 January 2013 | |
| ![](../../global_imgs/spacer.gif) | Related articles Composite Materials structuresLauncher StructuresSatellite StructuresStable Satellite StructuresComposite Joints and InsertsCeramicsComposite Technology Studies
|