Advanced sensory spacecraft structures
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 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