Vibration Test Prediction for a Telecom Satellite
Component-Wise Approach for Efficient and Accurate Analysis of Structures of Launchers
Predicting S/C Acoustic Tests Using the Boundary Element Method
Mechanical Testing on the Sun Calibration Mechanism for the MSI-VNS Instrument on EarthCARE
Effect of Carbon Nanotube Deformation on Electrical Properties of Carbon Nanotube Polymer Composites
Non-Conventional Carbon Nanotube Skeleton Reinforced Composites for Space Applications
Microvibrations in a 20 M Long Ka-Band SAR Interferometer
Variational Dynamic Coupled-Loads Analysis within the Frame of Launcher Upper Stage Development
Modes Interactions Due to Launcher Dynamic Behavior Variations During Flight
Consideration of Space Debris Issues in Early Spacecraft Design Phases
Design and Verification of Critical Pressurised Windows for Manned Spaceflight
Assembly of Space CFRP Structures with Racing Sailing Boats Technology
Assembly of Space CFRP Structures with Racing Sailing Boats Technology
Advanced Materials & Structural Concepts for Interstages Structures of Future Expendable Launchers
Structures, Material and Processes Technology in the Future Launchers Preparatory Program
The Boom Design of the De-Orbit Sail Satellite
Functional Analysis of Diaphragm Tanks and Testing of Primary Aspects Under Relevant Conditions
Experimental Evaluation of the Canadarm2 Residual Flexural Strength After an Orbital Debris Impact
The Development of Thermal Conductive RTM CFRP Technology for Space Applications
Vibro-Acoustic Response of the SWARM Satellite Through a Mode Count Procedure
Simulation of the Payload Fairing Behavior During Separation
Response of a Two-Panel System with Medium Modal Density by a Hybrid Method
Sandwich Cylinder Technology for Cryogenic Tank
Advanced Structural Optimization Under Consideration of Cost Tracking
Development of a Lightweight Segmented Deformable Mirror for High-Order Wavefront Control
VEGA Launch Vehicle Dynamic Environment: Flight Experience and Qualification Status
Robust Design of Notching Profiles Under Lack of Knowledge
Novel Hybrid Ablative/Ceramic Heatshield for Earth Atmospheric Re-Entry
Equivalent Viscous Damping Methodologies Applied on VEGA Launch Vehicle Numerical Model
Z40 Solid Rocket Motor: Design Status of the Motor Case Structure
Advanced Cryo-Tanks Structural Design Investigated in CHATT
Inflatable Rigidisable Mast for End-of-Life Deorbiting System
Design of the De-Orbit Sail Boom Deployment Unit