“…In particular, the linear transport terms for mass, viscosity, diffusion, and thermal conductivity in the partial differential equations are no longer valid (Prasanth and Kakkassery, 2006). For such problems it is necessary to implement the Boltzmann equation of kinetic energy, which can be used to consider the molecular transport phenomena across all Mach numbers and Knudsen numbers of rarefied gases, and as such it is considered the best approach to describe the hypersonic rarefied gas flows (e.g., Cercignani, 2000;Li et al, 2015). The most common application of the Boltzmann equation is in describing the conditions relevant to the problem of re-entry vehicles in the upper atmosphere, where hypersonic conditions in the rarefied flow produce ionizing reactions, and subsequently a thin plasma sheath which can block communications (e.g., Boyd, 2007aBoyd, , 2014Boyd et al, 2016).…”