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

    Papers

    1. NUMERICAL SIMULATION OF IMPACT LOADING ON ELASTIC SPACE STRUCTURE AND CASE STUDIES

    2. Designing Small Spacecraft to Operate in the Lunar Environment

    3. Influence Factors of Temperature Difference between Ground Thermal Balance Test and Orbit Data of Spacecraft

    4. Impact detection onboard satellites using wireless sensor network

    5. Development of Electron Emitting Film for Spacecraft Charging Mitigation II Improvement of Performance

    6. Investigation into Tolerance of Polysiloxane-Block-Polyimide Film against Atomic Oxygen

    7. Low CTE Waveguide for Extreme Thermal Environment

    8. A Small Low-Cost Resistance Based Atomic Oxygen Sensor

    9. Development Status and Prospect of TPS for RLV

    10. Analysis of the Long-Term Evolution of Satellite Temperatures by Analysing of its Thermal Behavior in Orbit

    11. development of spacecraft charging measuring instrument with parallel plate electrostatic energy analyzer