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  • VP. Virtual Presentations - IAF MATERIALS AND STRUCTURES SYMPOSIUM

    Papers

    1. cfd analysis of acoustic damping on Helmholtz resonators inside rockets combustion chambers.

    2. CubeSat thermal analysis and design: Techniques and reference guidelines for CubeSat developers

    3. Buffer and compliant reinforcement learning control of space robot capture spacecraft with compliant mechanism

    4. Burst pressure estimation considering the measured residual strain and 3-D profile of a Solid Rocket Motor hardware

    5. finite element analysis and vibration testing of the mysat-2 cubesat

    6. Carbon Nanotubes as Modifying Agent of Energetic Compositions: More Safety with Unaltered Applicability

    7. Research of Satellite Separation Attitude Based on Monte Carlo Method

    8. Anisotropic Heat-Shielding Materials: Prospects for Aplication in the Re-entry Module Heat Shield

    10. Integrated Thermal Protection System Design for Hypersonic Vehicle Based on New Thermal-Mechanical Method

    11. aerodynamic heating reduction with jet arrays over the sharp edge of a hypersonic vehicle

    12. 3D printed composite assessment by hyperspectral analysis

    13. 3D printed copper – graphene oxide composites

    14. Photovoltaic Solar Cells.

    16. tardigrade mech: boron nitride nanotube composites for space radiation protection

    17. carbon fiber reinforced plastics with aluminum honeycomb core design methodology for space and surface mining applications

    20. low cost filament-winding technology for small aerospace laboratories and startups

    21. multi-objective optimization of a small launch vehicle aerodynamic payload fairing for minimum drag and mass

    22. new structure for body-mounted solar array satellite

    23. An Analytical Approach for Large Size Optimised Reinforced Hole in Composite Circular Cylindrical Shells

    24. Studies on Lunar Lander stability behaviour using a 1/6th Scale Model

    25. Design, Development and Qualification Testing of a High Pressure Gas Bottle for a Cryogenic Rocket Stage.