Load Derivation
Tracks
Newton 1
| Thursday, May 31, 2018 |
| 4:30 PM - 6:30 PM |
| Newton 1 |
Details
Chairs: Werner Konrad (Airbus), Benoit Tang (CNES)
Speaker
Attendee94
Structural Engineer
ESA - ESTEC
Prediction of the Mechanical Environments of the Load Critical Elements of the ATHENA Spacecraft
Attendee610
Politecnico Di Torino - DIMEAS
Local Refinement of Classical FEM Solutions Using Elements with Node-Dependent Kinematics
Attendee358
Ariane Group
Consistent Dimensioning Interface Loads – An Alternative and Less Conservative Approach to Define Loads for Sub-Components
Attendee102
Airbus Defence And Space GmbH
Diversity of Random Vibration Load Definition from Early Phase to Testing Using the Example of Sentinel-2 S/C
