Mixture Ratio Optimization
Mixture Ratio Optimization is a method in liquid rocket engine design that determines the optimal proportion of oxidizer to fuel in the propellant mixture to maximize performance metrics such as specific impulse while balancing thermal and operational constraints.
104
Publications
3.8K
Citations
441
Authors
177
Institutions
Publications per year
2017–2026
55
Parents
104
Combustion of Nanoscale Al/MoO3 Thermite in Microchannels
Steven F. Son, B. W. Asay, Timothy J. Foley et al. · Journal of Propulsion and Power · 2007 · 181 citations
Omar I. Awad, Rizalman Mamat, Obed M. Ali et al. · Energy Conversion and Management · 2017 · 157 citations · Full text
Engineering, Automotive Engineering, Chemical Engineering +17
Junfei Zhang, Yimiao Huang, Guowei Ma et al. · Resources Conservation and Recycling · 2021 · 127 citations · Full text
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177

Central South University
Changsha, China
3 h-index
8 publications
198 citations

Sidi Mohamed Ben Abdellah University
Fes, Morocco
2 h-index
5 publications
219 citations
Université Ibn-Tofail
Kenitra, Morocco
2 h-index
6 publications
314 citations
RWTH Aachen University
Aachen, Germany
2 h-index
4 publications
163 citations
Politecnico di Torino
Turin, Italy
2 h-index
3 publications
168 citations
Los Alamos National Laboratory
Los Alamos, United States
2 h-index
6 publications
615 citations

Universiti Sains Malaysia
George Town, Malaysia
2 h-index
3 publications
294 citations
Tsinghua University
Beijing, China
2 h-index
9 publications
2.5K citations
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6 publications · 104 citations
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4 publications · 68 citations
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3 publications · 102 citations
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3 publications · 168 citations
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3 publications · 224 citations
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