rootbrowseIAC-14C2session 77. Space Vehicles – Mechanical/Thermal/Fluidic SystemsPapers1. CONCEPTUALIZATION OF DESIGN MODIFICATIONS IN RE-ENTRY VEHICLES - VECTORING FOR REDIRECTION OF PLASMA2. Heat Transfer Management by Aerospikes for a Hypothesized Lifting Body in Hypersonic Flow3. lift-to-drag ratio requirement analysis including low altitude guidance for re-entry flight of vtol vehicle4. The 3 Omega Transient Line Method for Thermal Characterization of Superinsulator Materials Developed for Spacecraft Thermal Control5. Low orbit environment effects on Carbon/SiC composites: experimental and numerical approach6. Thermo-Mechanical Concept for a Modular On-Orbit-Serviceable Satellite System7. design, build and experimental study of emergency power assist system8. Parametric tool for the thermal analysis of a satellite.9. active thermal control system for venusian lander. new proposal10. Potential advantages of the Space Vehicles with nuclear power - plant on board when dealing with global problems of modern age11. Conceptual Design of a new Hybrid Capsule for manned Atmospheric Re-entry applications12. Investigation of Heatshield Shape Changes on Optimum Aerodynamic Design for a Mars Entry Capsule13. characterization of high intensity sun radiation for tv-tb testing in a large vacuum facility