The erosion of polymers and polymer-based materials (such as composites and
paints) due to atomic oxygen (AO) present in the low Earth orbit (LEO) env
ironment is described. Since many polymers are used extensively to fabricat
e spacecraft structures and components, a method of protecting them from AO
erosion was developed. This process involves surface activation of the pol
ymer by UV radiation and subsequent silylation treatment to produce an oute
r layer (not a coating) of silicon-dioxide based material. Experiments cond
ucted in the UTIAS AO beam facility provide comparative test data for a wid
e range of polymers, including composites and polyurethane paints. A predic
tive model is also presented for estimating the AO erosion rates for hydroc
arbon polymers based on their polymer repeat unit structure.