Rocket Nozzle Inserts
Rocket Nozzle Insert is a specialized component fabricated from carbon-carbon composite materials designed to line the throat or convergence zone of a rocket nozzle, providing thermal and structural resistance against high-velocity, high-temperature exhaust flows during propulsion.
12
Publications
536
Citations
43
Authors
24
Institutions
Publications per year
2017–2026
5
Parents
12
Matthew B. Dickerson, P. J. Wurm, J. R. Schorr et al. · Journal of Materials Science · 2004 · 98 citations
Testing ultra-high-temperature ceramics for thermal protection and rocket applications
Raffaele Savino, Stefano Mungiguerra, Giuseppe D. Di Martino · Advances in Applied Ceramics Structural Functional and Bioceramics · 2018 · 35 citations · Full text
Engineering, Aerospace Engineering, Materials Engineering +17
1–5 of 12
43
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Missouri University of Science and Technology, United States
1 publications · 141 citations
1
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1
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1–5 of 43
24

Sapienza University of Rome
Rome, Italy
1 h-index
1 publications
32 citations
Instituto Nacional de Técnica Aeroespacial
Madrid, Spain
1 h-index
1 publications
20 citations

Université Toulouse III - Paul Sabatier
Toulouse, France
1 h-index
3 publications
66 citations
Georgia Institute of Technology
Atlanta, United States
1 h-index
2 publications
196 citations
Missouri University of Science and Technology
Rolla, United States
1 h-index
2 publications
282 citations

Moscow Aviation Institute
Moscow, Russia
1 h-index
1 publications
16 citations

National University of Defense Technology
Changsha, China
1 h-index
8 publications
232 citations

Université Fédérale de Toulouse Midi-Pyrénées
Toulouse, France
1 h-index
3 publications
66 citations
1–8 of 24
AST · 2 publications · 49 citations
2
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2 publications · 38 citations
2
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2 publications · 127 citations
2
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1 publications · 98 citations
1
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Repository · 1 publications · 14 citations
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