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  • session 6
  • 6. Space Environmental Effects and Spacecraft Protection

    Papers

    1. Effects of space thermal-vacuum conditions on the electromagnetic reflectivity of small satellites structural plates

    2. Test campaign to determine the properties and space durability of an electrodynamic low work function tether

    3. Mitigating Lunar Dust on Spacecraft Surfaces Using Electromagnetic Fields

    6. Whipple Shielding Spacecraft using Ni-Ti Shape Memory Alloy and Aerogel Composite.

    8. Early Results from the DISCOVERER Project

    9. HEATING OF TELESCOPE STRUCTURE DUE TO REFLECTED SUNLIGHT FROM TELESCOPE OPTICS

    10. Aerogel based thermal insulation and UV resistant system for moon and mars settlement

    11. THE MODELLING OF THE DEGRADATION AND LIFETIME ESTIMATION FOR THE GEO SATELLITES SURFACE MATERIAL BY ITS PHOTOMETRIC OBSERVATIONS AND LABORATORY DATA

    12. Determination of spacecraft attitude based on the heat flux analysis

    1004. acoustic radiation sources analysis during launch vehicle lift-off with different gas ducts

    1005. The Radiation Environment and effects analysis of the LUMIO Mission.

    1007. shielding evaluation of polyethylene/regolith composites in the martian radiation environment