rootbrowseIAC-08C2session 66. Space Environmental Effects and Spacecraft ProtectionPapers1. NUMERICAL SIMULATION OF IMPACT LOADING ON ELASTIC SPACE STRUCTURE AND CASE STUDIES2. Designing Small Spacecraft to Operate in the Lunar Environment3. Influence Factors of Temperature Difference between Ground Thermal Balance Test and Orbit Data of Spacecraft4. Impact detection onboard satellites using wireless sensor network5. Development of Electron Emitting Film for Spacecraft Charging Mitigation II Improvement of Performance6. Investigation into Tolerance of Polysiloxane-Block-Polyimide Film against Atomic Oxygen7. Low CTE Waveguide for Extreme Thermal Environment8. A Small Low-Cost Resistance Based Atomic Oxygen Sensor9. Development Status and Prospect of TPS for RLV10. Analysis of the Long-Term Evolution of Satellite Temperatures by Analysing of its Thermal Behavior in Orbit11. development of spacecraft charging measuring instrument with parallel plate electrostatic energy analyzer