rootbrowseIAC-19C2session IPIP. Interactive Presentations - IAF MATERIALS AND STRUCTURES SYMPOSIUMPapers1. surface functionalization of graphene prior to nanoparticles tethering for tri-functionality in both acidic and alkaline media2. On-Orbit Additive Manufacturing of Parabolic Reflectors via Solar Photopolymerization3. Ground simulation system for active vibration control based on the bio-inspired X-shape structure for free-floating spacecraft4. Wind Tunnel Data Analyzing by Javad Software5. optimizing topology and stacking sequence in laminated composite structures6. BASE ANALOG TO MARS Ice as a parametric insulation facade7. Environmental analysis of nanorovers in a swarm for lunar's scientific missions8. Analysis of influences of external components during vibration testing of CubeSats9. Vibration test for 7 ton-class liquid propellant rocket engine10. The beneficiation of lunar regolith using electrostatic separation for Space Resource Utilisation11. High Temperature Thermal Margin12. Integration of a Reaction Wheel System into a Sounding Rocket to Increase Stability and Performance13. Thermal and Structural Optimization of Small Satellites using Composite Materials14. Analysis of an Additive Manufactured Liquid Rocket Engine15. Sensor coatings for high-temperature measurements in space applications16. Development of Artificial Exterior Skin for Remote Robotics17. Optimal Design of the Back Truss Structure for Minimizing the Deformation of Reflector under Gravity18. The influence of union design in thrust measurement of A to D category rocket motor in an amateur test bench. A case study19. Multi-Objective optimization of a Small Launch Vehicle Aerodynamic Payload Fairing for Minimum Drag and Mass.20. Impact Properties of Micro-Channeled Epoxy Foams and Fiber Reinforced Micro-Channeled Composites21. PW-SAT2 DEORBIT SAIL TEST CAMPAIGN AT DROP TOWER and verification on orbit. analysis of impact damage on stiffened composite panels of spacecraft. MATHEMATICAL MODELING OF THIN ABLATING THERMAL PROTECTION COVERING. Optimizing the Geometric Parameters of a Space Module’s Outer Shell during a Rocket’s Flight Sequence. Orbital space testing platform designed to enable new technologies. Thermal-Vacuum Testing Campaign of the CBERS-4A Satellite Performed at INPE, Brazil