KRP Mechatec GmbH
info@krp-m.de
+49 (0)151 1461 2442
Suche
We speak the following languages:
Menu
Home
Company
Our Business Segments
About us
Our Team
Downloads
Services
Test
Analyses
Engineering
Projects
Space
Aviation
Fusion
Other Industries
Programs
Contact
Design & Analysis of a Star Sensor Bracket
Home
/
Projects
/
Space
/
Design & Analysis of a Star Sensor Bracket
CAD model
FEM model
Design and analysis of a ceramic (HB-Cesic®) star sensor bracket for Meteosat Third Generation Satellite
Design optimization for mass minimization and minimization of thermo-elastic deformations
Performance of all FE analyses and verifications for the qualification of the sensor bracket:
Quasistatic analyses
Modal analyses
Sinus- and random vibration analyses
Thermale analyses
Thermo-elastic analyses
Planning and performance of all qualifikationstests
Project details
Core competencies:
Space
Program:
MTG
next item
More interesting projects
Specification of the Random Vibration Spectrum for the MERTIS Bolometer
Stability Test of Aicraft Floor-Panels
Determination of Material Properties of Additive Layer Manufacturing Aluminium and Titanium Alloy Specimens at Low Temperatures
Biaxial load test of ITER Vacuum Vessel Support
Development of a CFRP Floor Panel for a Cargo Aircraft
Life Cycle Tests of NSE-Connection-Elements for the Wendelstein W7-X Fusion Experiment
Thermal Vacuum and Thermal Balance Testing for a Highly Stable Star-Sensor-Bracket
Copyright © 2023 KRP Mechatec GmbH
Scroll