Energy relaxation in superthermal collisions of carbon with oxygen: the influence of isotopic substitution

TL;DR

This study provides detailed potential energy curves and cross sections for carbon-oxygen collisions, highlighting the importance of isotopic variations in modeling Martian atmospheric escape.

Contribution

The paper introduces highly accurate PECs and cross sections for C($^3$P) + O($^3$P) collisions, including isotopic effects, improving modeling of planetary atmospheric loss.

Findings

Cross sections involving carbon differ by up to a factor of two from oxygen proxies.

Isotopic variations in collisions can cause up to 8% differences in cross sections.

Even moderate isotopic effects significantly impact Martian atmospheric escape models.

Abstract

The transition from a once-dense Martian atmosphere to the thin one observed today implies a substantial loss of carbon, either through atmospheric escape or surface deposition. Accurately modeling this carbon escape necessitates accounting for collisions between energetic carbon atoms and the primary atmospheric constituents, including oxygen. To this end, we computed a highly accurate and comprehensive set of potential energy curves (PECs) for the C($^3$P) + O($^3$P) system. Based on these PECs, we derived statistically averaged total elastic and differential cross sections. Comparison with literature data for O($^3$P) + O($^3$P) collisions reveals that cross sections involving carbon can differ by up to a factor of two, indicating that oxygen is not a good proxy for modeling carbon escape. Furthermore, we evaluated the impact of all possible isotopic combinations in C($^3$P) + O($^3$P) collisions and found variations in cross sections of up to 8\%. Given the observed isotopic enrichment of carbon and oxygen in the Martian atmosphere, even such moderate differences can have a significant effect on escape models and the interpretation of planetary evolution.