Mass flux and current density distributions of electrospray plumes
Author:
Affiliation:
1. Plasma & Space Propulsion Laboratory, Department of Mechanical and Aerospace Engineering, University of California, Los Angeles, 420 Westwood Plaza, Los Angeles, California 90095, USA
Funder
Jet Propulsion Laboratory
Air Force Research Laboratory
Air Force Office of Scientific Research
National Aeronautics and Space Administration
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0056761
Reference24 articles.
1. Lifetime Considerations for Electrospray Thrusters
2. R. E. Wirz, A. L. Collins, A. Thuppul, P. L. Wright, N. M. Uchizono, H. Huh, M. J. Davis, J. K. Ziemer, and N. K. Demmons, “Electrospray thruster performance and lifetime investigation for the LISA mission,” in AIAA Propulsion and Energy 2019 Forum, Indianapolis, IN (American Institute of Aeronautics and Astronautics, 2019), p. 3816.
3. 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 (Electric Rocket Propulsion Society, 2020), p. 3609.
4. Emission Modes in Electrospray Thrusters Operating with High Conductivity Ionic Liquids
5. Polyatomic Ion-Induced Electron Emission (IIEE) in Electrospray Thrusters
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