Modeling and Characterization of Electrospray Propellant-Surface Interactions
Author:
Affiliation:
1. Massachusetts Institute of Technology,Cambridge,MA,02139
2. Cornell University,Ithaca,NY,14853
3. Technical University of Munich,Munich,Germany,85748
Funder
NASA
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9843190/9843194/09843583.pdf?arnumber=9843583
Reference29 articles.
1. Polyatomic Ion-Induced Electron Emission (IIEE) in Electrospray Thrusters
2. Ion-induced electron emission from emim-bf4 electro spray plume-surface interactions;klosterman;AIAA Scitech 2021 Forum,2021
3. Kinetic Plume Modeling of Electrospray Pure Ion Emission;petro;Journal of Applied Physics,2021
4. A hierarchical O(N log N) force-calculation algorithm
5. Fast Parallel Algorithms for Short-Range Molecular Dynamics
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3. Angular Properties of Ionic Liquid Electrospray Emitters;AIAA SCITECH 2023 Forum;2023-01-19
4. Comparison of computational algorithms for simulating an electrospray plume with a n-body approach;Journal of Electric Propulsion;2022-10-07
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