Full-gap kinetic limitation of thermionic-electron transport for electron transpiration cooling
Wushun Zhang, Weixing Zhou, Yinjian Zhao

TL;DR
This paper develops a detailed kinetic model to understand how thermionic electron emission and backflow affect electron transpiration cooling efficiency in hypersonic applications.
Contribution
It introduces a comprehensive PIC-MCC simulation framework that captures the full kinetic processes governing electron escape and backflow in thermionic-electron transport.
Findings
Identifies a sharp transition to backflow-limited transport at specific emission levels.
Shows that increased emission can lead to higher boundary energy diagnostics but not improved electron escape.
Quantifies backflow ratio reaching over 54% at the transition point.
Abstract
Electron transpiration cooling (ETC) can reduce aerothermal loads on sharp hypersonic leading edges, but its performance is governed by whether thermionically emitted electrons escape the hot surface or return as cathode-directed backflow. Here, a one-dimensional-in-space, three-dimensional-in-velocity electrostatic particle-in-cell/Monte Carlo collision model is developed for a full cathode--anode plasma diode, resolving thermionic emission, collisional plasma transport, emitted-electron backflow, and downstream collection. A helium benchmark is used to examine emitted-electron transport and backflow-limited current flow. With increasing imposed emission, the diode first remains in a weak-backflow regime, where net emitted-electron transport and downstream collection both increase with emission. Further increasing the emission produces a sharp transition to backflow-limited transport…
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