Multiscale modeling of electrospray ion emission
Author:
Affiliation:
1. Sibley School of Mechanical and Aerospace Engineering, Cornell University, Ithaca, New York 14850, USA
2. Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139, USA
Abstract
Funder
National Aeronautics and Space Administration
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0065615
Reference43 articles.
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2. Electrospray ionization-principles and practice
3. Nanoengineered thrusters for the next giant leap in space exploration
4. E. Petro, A. Bruno, P. Lozano, L. E. Perna, and D. Freeman, “Characterization of the TILE electrospray emitters,” in AIAA Propulsion and Energy 2020 Forum (AIAA, 2020), p. 3612.
5. J. K. Ziemer, C. Marrese-Reading, S. Arestie, N. R. Demmons, R. E. Wirz, A. Collins, and M. Gamero, “Progress on developing LISA microthruster technology,” in AIAA Propulsion and Energy 2020 Forum (AIAA, 2020), p. 3609.
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