Modeling of an ionic liquid electrospray using molecular dynamics with constraints.

Arnaud Borner1, Zheng Li, Deborah A Levin

  • 1Department of Aerospace Engineering, The Pennsylvania State University, University Park, Pennsylvania 16802, USA. apb170@psu.edu

Summary

Molecular dynamics simulations revealed the behavior of EMIM-BF(4) ionic liquid under electrospray thruster conditions. A threshold electric field of 1.2 V/nm was identified for particle emission, crucial for thruster design.

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