Abstract
Molecular dynamics (MD) simulations are performed to model an electrospray thruster for the ionic liquid (IL) EMIM-BF4 using an effective-force coarse-grained potential. The MD simulations provide insight into the atomistic modeling of a capillary-tip-extractor system, the basic elements of an electrospray thruster. A 1-D electric field showed an improvement in the model when compared with the use of a constant electric field. Then, the MD software was coupled to a Poisson solver derived from a particle-in-cell code. A transient 3-D electric field was used at each timestep, taking into account the induced electric field due to space charge repulsion. It was found that the inhomogeneous electric field as well as that of the IL space-charge improved agreement between modeling and experiment. The influence of numerical parameters, such as extraction potential and applied mass flow, was studied. Particular emphasis was put on the importance of parameters relative to the grid used to solve Poisson's equation, such as the grid cell size and the boundary conditions (BCs) in the vicinity of the capillary tip. The BCs were found to have a substantial impact on the potential and electric field.
Original language | English (US) |
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Article number | 6840344 |
Pages (from-to) | 295-304 |
Number of pages | 10 |
Journal | IEEE Transactions on Plasma Science |
Volume | 43 |
Issue number | 1 |
DOIs | |
State | Published - Jan 1 2015 |
Externally published | Yes |
Keywords
- Boundary conditions
- finite difference methods
- ion emission
- molecular computing
- parallel algorithms
- plasma chemistry
ASJC Scopus subject areas
- Nuclear and High Energy Physics
- Condensed Matter Physics