- Planning, performance (at the Space Test Center IABG) and evaluation of vibration tests for ceramic (HB-Cesic®) star sensor bracket for Meteosat Third Generation Satellite
- Performance of qualification as well as acceptance testing for flight models
- Sine and random vibration tests
- Experimental approximation of interface loads (forces/moments) based on a reduced mass matrix (Guyan reduction of FE model to the acceleration sensor positions) and the measured accelerations for sine as well as random vibration tests (mass operator method, see ECSS-E-HB-32-26A)
- Computation and verification of notching profiles based on the approximated interface loads (see above) for sine and random vibration tests
- Corellation of test results with FE analyis results
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Fatigue Tests and Determination of the Mechanical and Thermal Properties of Electro-Deposed Copper for the Accelerator Grid (SPIDER) -
Structural-Mechanical and Thermal FEM Analysis of the EnMAP Calibration Unit -
Specification of the Random Vibration Spectrum for the MERTIS Bolometer -
Thermal-Vacuum test for an Endoscope for the Fusion Experiment Joint European Torus (JET) -
Mechanical Testing of Components of Cryogenic Hydrogen Tank -
FEM analyses of the waveguides for MetOp-SG (Meteorological Operational Satellite - Second Generation) -
Functional and life tests of the ExoMars Crushing Station at Mars environmental conditions
KRP Mechatec GmbH is an engineering services provider specialized in structural tests and analyses in the field of space, aviation, experimental research and other high-tech industries, certified according to DIN EN ISO 9001:2015.
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