Rocket Nozzle Performance is a quantitative metric that evaluates the efficiency of a rocket nozzle in converting thermal energy from propellant combustion into directed kinetic energy of the exhaust jet, typically measured by parameters such as thrust coefficient, specific impulse, or characteristic velocity under defined operating conditions.
81
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2.2K
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224
Authors
80
Institutions
Publications per year
2017–2026
20
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Publications
81
Recent Advances in Gas-Particle Nozzle Flows
R. F. Hoglund · ARS journal · 1962 · 107 citations
Engineering, Aerospace Engineering, Mechanical Engineering +16
The Fluid Mechanics of Pulsed Laser Propulsion
Girard A. Simons, A. N. Pirri · AIAA Journal · 1977 · 94 citations
1–5 of 81
Authors
224
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1–5 of 224
Institutions
80
Glenn Research Center
Cleveland, United States
7 h-index
11 publications
177 citations
Pennsylvania State University
State College, United States
3 h-index
7 publications
163 citations
Boeing (United States)
Chicago, United States
3 h-index
7 publications
212 citations
Langley Research Center
Hampton, United States
3 h-index
13 publications
337 citations
Beihang University
Beijing, China
3 h-index
14 publications
412 citations
University of Naples Federico II
Naples, Italy
3 h-index
7 publications
248 citations
Sapienza University of Rome
Rome, Italy
3 h-index
7 publications
367 citations
Jet Propulsion Laboratory
Pasadena, United States
2 h-index
3 publications
122 citations
1–8 of 80
Venues
- Journal of Propulsion and Power
9 publications · 371 citations
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- Journal of Spacecraft and Rockets
6 publications · 196 citations
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- Acta Astronautica
6 publications · 138 citations
6
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- Aerospace Science and Technology
AST · 5 publications · 132 citations
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- NASA Technical Reports Server (NASA)
Repository · 5 publications · 131 citations
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