Abstract
Fluorinated ethylene propylene (Teflon FEP) was used as external layer thermal insulator for Hubble Space Telescope (HST) and on the outside surfaces of space crafts in the low earth orbit (LEO). Teflon FEP was eroding as a result of exposure to atomic oxygen (AO) and different electromagnetic waves such as ultraviolet radiation and X-ray. Model molecules were used to simulate Teflon FEP and its interaction with other nanoparticles such as ZnO and SiO2. Density functional theory (DFT) was used to calculate model structures using B3LYP/LAN2DZ model. Molecular electrostatic potential as contour, band gap energy, and total dipole moment were computed for all models. Thermal stability properties were also studied for Teflon FEP both individually and interacted with ZnO and SiO2. Results showed that a layer of OZn and SiO2 on Teflon FEP, especially Teflon FEP + OZn + OSiO structure, improves the physical, chemical, thermal, and electrical stability of Teflon FEP, potentially acting as a corrosion-inhibiting layer.