Author:
Enomoto Takaaki,Parmar Shehan M.,Yamada Ryohei,Wirz Richard E.,Takao Yoshinori
Abstract
AbstractMolecular dynamics (MD) simulations were performed for ion extraction from electrospray thrusters to investigate relevant extraction processes numerically. To approximate the electrospray jet tip, a simulation domain consisting of 4-5 nm-sized ionic liquid droplets was used. The extracted ion angles and kinetic energies from EMI–BF4 (1-ethyl-3-methylimidazolium tetrafluoroborate) and EMI–Im (1-ethyl-3-methylimidazolium bis((trifluoromethyl)sulfonyl)imide) droplets were quantified by applying uniform electric fields of 1.3–1.7 V nm−1. The MD simulations are in great agreement with simulations presented in the literature and consistently show a greater preference for monomer emission than reported experimentally. At field strengths above 1.5 V nm−1, apparent droplet fracturing and breakup lead to an increase in ion angular velocity distributions. Greater mobility of EMI–BF4 ions than EMI–Im was also observed, indicative of the crucial role of cation-anion hydrogen bond strengths in ion extraction and beam composition between different propellants.
Funder
JSPS (Japan Society for the Promotion of Science) KAKENHI
Canon Foundation
Asahi Glass Foundation
SEI Group CSR Foundation
Yokohamakogyokai Research Aid Foundation
JAXA/RDD
U.S. Department of Energy, Office of Science, Office of Advanced Scientific Computing Research,
NASA’s Jet Propulsion Laboratory, California Institute of Technology
Air Force Office of Scientific Research
Publisher
Springer Science and Business Media LLC
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