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  • session 7
  • 7. Space Vehicles – Mechanical/Thermal/Fluidic Systems

    Papers

    1. CONCEPTUALIZATION OF DESIGN MODIFICATIONS IN RE-ENTRY VEHICLES - VECTORING FOR REDIRECTION OF PLASMA

    2. Heat Transfer Management by Aerospikes for a Hypothesized Lifting Body in Hypersonic Flow

    3. lift-to-drag ratio requirement analysis including low altitude guidance for re-entry flight of vtol vehicle

    4. The 3 Omega Transient Line Method for Thermal Characterization of Superinsulator Materials Developed for Spacecraft Thermal Control

    5. Low orbit environment effects on Carbon/SiC composites: experimental and numerical approach

    6. Thermo-Mechanical Concept for a Modular On-Orbit-Serviceable Satellite System

    7. design, build and experimental study of emergency power assist system

    8. Parametric tool for the thermal analysis of a satellite.

    9. active thermal control system for venusian lander. new proposal

    10. Potential advantages of the Space Vehicles with nuclear power - plant on board when dealing with global problems of modern age

    11. Conceptual Design of a new Hybrid Capsule for manned Atmospheric Re-entry applications

    12. Investigation of Heatshield Shape Changes on Optimum Aerodynamic Design for a Mars Entry Capsule

    13. characterization of high intensity sun radiation for tv-tb testing in a large vacuum facility