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Computational modeling reveals that hyperthermal ground-state atomic oxygen disrupts alkane chains under low Earth orbit conditions, indicating accelerated erosion of spacecraft polyethylene.
O(3P) is a highly reactive species which may cause damage to materials on contact. In low Earth orbit (LEO), high-energy collisions (∼4.5 eV) of O(3P) with spacecraft materials can lead to extensive degradation. In this study, we use ab initio molecular orbital calculations to investigate the possibility of chain breaking in polyethylene caused by a single O(3P) attack under LEO conditions, because the occurrence of such reactions could greatly accelerate the erosion. The smallest alkanes ( n = 2, 3, 5, or 7) serve as models of polyethylene. For the case of ethane ( n = 2), we explore the triplet potential energy surface of the following reaction: O(3P) + CH 3 −CH 3 → ·O−CH 3 + ·CH 3 . Analogous reactions, in which O(3P) attacks a central carbon atom, are studied for the higher alkanes. Results obtained using the Hartree−Fock method, density functional theory, and, in the simplest case (i.e., ethane), second-order Möller−Plesset perturbation theory, Gaussian theoretical models (G1, G2, and G2MP2), and complete basis set (CBS-QB3) approaches are reported. We conclude that conditions in LEO are conducive to chain breaking in polyethylene caused by a single O(3P) attack.
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Gindulytė et al. (2000) studied this question.
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