Ablative Nozzle is a type of rocket nozzle constructed from composite materials designed to dissipate intense thermal loads during high-speed propulsion by controlled surface erosion, thereby maintaining structural integrity through sacrificial material loss.
27
Publications
945
Citations
79
Authors
31
Institutions
Publications per year
2017–2026
11
Parents
Publications
27
Ablation of the carbon/carbon composite nozzle-throats in a small solid rocket motor
Kezhi Li, Xuetao Shen, Hejun Li et al. · Carbon · 2010 · 144 citations
Ablative Laser Propulsion: An Old Concept Revisited
Andrew V. Pakhomov, Don A. Gregory · AIAA Journal · 2000 · 80 citations
Natural Sciences, Physics, Optics +13
1–5 of 27
Authors
79
- LP
2
h-index
- DB
2
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- RY
2
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- GC
2
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- FQ
2
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1–5 of 79
Institutions
31
Northwestern Polytechnical University
Xi'an, China
7 h-index
29 publications
1.5K citations
Beihang University
Beijing, China
3 h-index
15 publications
480 citations
University of Alabama in Huntsville
Huntsville, United States
3 h-index
7 publications
251 citations
Sapienza University of Rome
Rome, Italy
2 h-index
4 publications
251 citations
Commissariat à l'Énergie Atomique et aux Énergies Alternatives
Paris, France
1 h-index
2 publications
264 citations
Korea Advanced Institute of Science and Technology
Daejeon, South Korea
1 h-index
3 publications
132 citations
Office National d'Études et de Recherches Aérospatiales
Palaiseau, France
1 h-index
1 publications
20 citations
Université Toulouse III - Paul Sabatier
Toulouse, France
1 h-index
2 publications
264 citations
1–8 of 31
Venues
- Aerospace Science and Technology
AST · 2 publications · 60 citations
3
h-index
- AIAA Journal
3 publications · 107 citations
3
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- Acta Astronautica
3 publications · 98 citations
3
h-index
- Carbon
3 publications · 235 citations
3
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- International Journal of Applied Ceramic Technology
1 publications · 13 citations
1
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