Trends in Oil Spills from Tankers and ITOPF Non-tanker Attended Incidents
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
Real Time Visualisation of Cleanroom Conditions
Additive Layer Manufacturing for Launcher's Applications
SmallGEO Structural-Thermal Model (STM) Mechanical Test Campaign
How to Improve the Speed of Vibro-Acoustic Simulations?
Application of a Substructural Method for Modelling Satellite Microvibrations
A Complex Mode Approach for the Validation of FE Models with Structural Damping
Modal Identification and Correlation of a FEM with Test Data Using Primodal
Modal Frequency Adjustment of the Eu:CROPIS Satellite Structure
High Stability Optical Mount for Space Laser Applications
Fracture Control and Damage Tolerance Methods for Highly Loaded Launcher Components
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
Design and Analysis of Heliogyro Sail Deployment System
Solar Sail Membrane Testing and Design Considerations