Electrothermal Propulsion
Electrothermal Propulsion is a type of electric propulsion system in which thermal energy is added to a propellant through electrical heating, thereby increasing its enthalpy and enabling acceleration through a nozzle to produce thrust.
95
Publications
4.2K
Citations
284
Authors
101
Institutions
Publications per year
2017–2026
20
Parents
95
Physics of Electric Propulsion
R. G. Jahn, F. A. Lyman · Journal of Applied Mechanics · 1969 · 837 citations · Full text
Technology of closed-drift thrusters
H. R. Kaufman · AIAA Journal · 1985 · 116 citations
1–5 of 95
284
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National Institute of Information and Communications Technology, Japan
4 publications · 100 citations
4
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1–5 of 284
101

Glenn Research Center
Cleveland, United States
9 h-index
12 publications
248 citations

Kyoto University
Kyoto, Japan
6 h-index
23 publications
641 citations
The Aerospace Corporation
El Segundo, United States
4 h-index
12 publications
261 citations

Pennsylvania State University
State College, United States
3 h-index
8 publications
194 citations
Jet Propulsion Laboratory
Pasadena, United States
3 h-index
7 publications
181 citations
University of Michigan
Ann Arbor, United States
3 h-index
6 publications
186 citations
Princeton University
Princeton, United States
2 h-index
4 publications
112 citations

Australian National University
Canberra, Australia
2 h-index
5 publications
169 citations
1–8 of 101
14 publications · 429 citations
13
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5 publications · 94 citations
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3 publications · 286 citations
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3 publications · 217 citations
3
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2 publications · 56 citations
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