- 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
-
Support of the Qualification of a Helicopter Liferaft-System -
Thermal Vacuum and Thermal Balance Testing for a Highly Stable Star-Sensor-Bracket -
Permeability Test for CFRP Membranes in Cryogenic Conditions -
Optimal Support-Positioning of M1-Mirror-Segments of E-ELT -
Life Cycle Tests of NSE-Connection-Elements for the Wendelstein W7-X Fusion Experiment -
Multi-Axis Force- and Moment-Load Test of a Hold Down Mechanism During Launch Phase -
Fatigue Tests and Determination of the Mechanical and Thermal Properties of Electro-Deposed Copper for the Accelerator Grid (SPIDER)
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.
KRP Mechatec GmbH Boltzmannstr. 2 85748 Garching | ||
Telefon Telefax E-Mail Internet | +49 (0)151 1461 2442 +49 (0)8131 505 331 info@krp-m.de | |
Copyright © 2023 KRP Mechatec GmbH