Advanced sensory spacecraft structures
Overview of the NASA Advanced Composite Solar Sail (ACS3) Technology Demonstration Project
Advanced Manufacturing Methods for Systems of Microsystem Nanospacecraft - Status of the Project
Self-Folding Smart Structure Inspired by Nature's Heliotropism
Large Folded, Deployable Structure Development
Structural Concept Selection for the DeployTech / Gossamer-2 Boom Deployment Mechanism
New Rotary Table Providing Improved Mass Property Measurements
Frequency Domain Compensation Method for Moving Part Disturbance Measurement
The SRS-Viewer: A Software Tool for Displaying and Evaluation of Pyroshock Data
ExoMars MSA. Testing Activities for EDM Separation Performance Verification
Sun Simulation at High Flux Level
Use of Virtual Testing for Equipments Qualification Tests and Thermal Model Validation Improvement
Mathematical Models of IABG Thermal-Vacuum Facilities
Heat Transfer Mathematical Model of Satellite Based on Thermal Tests and Inverse Problems Technique
Shock Isolation on Planet Mars
Design of Launcher Towards Spacecraft Comfort: Ariane 6 Objectives
VEGA Launch Vehicle Vibro-Acoustic Approach for Multi Payload Configuration Qualification
Behaviour of High Pressure Vessel Under an Hypervelocity Impact
Simulation of Satellite Vibration Test
Damping in Space Constructions
Design, Development and Manufacturing of the IXV Aeroshell Panels
Landing System Development - Design and Test Prediction of a Lander Leg Using Nonlinear Analysis
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