Propellant Heating Systems
Propellant Heating System is a nuclear thermal propulsion subsystem that belongs to the class of spacecraft propulsion technologies and is specifically characterized by its function of transferring thermal energy from a nuclear reactor to a propellant to increase its enthalpy and generate thrust through expansion in a nozzle.
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300
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10
Institutions
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2017–2026
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Korea Advanced Institute of Science and Technology
Daejeon, South Korea
1 h-index
3 publications
30 citations
University of Idaho
Moscow, United States
1 h-index
1 publications
72 citations
Daimler (Germany)
Stuttgart, Germany
1 h-index
3 publications
30 citations
Institut de Mécanique des Fluides de Toulouse
Toulouse, France
1 h-index
1 publications
15 citations
Marshall Space Flight Center
Redstone Arsenal, United States
1 h-index
1 publications
22 citations
California Institute of Technology
Pasadena, United States
1 h-index
2 publications
108 citations

Glenn Research Center
Cleveland, United States
1 h-index
2 publications
24 citations
National University of Singapore
Singapore, Singapore
1 h-index
5 publications
345 citations
1–8 of 10
1 publications · 15 citations
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Conference · 1 publications · 22 citations
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1 publications · 72 citations
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1 publications · 69 citations
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Conference · 1 publications · 10 citations
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