Spacecraft Structural Optimization
Spacecraft Structural Optimization is a computational engineering methodology that systematically minimizes mass, maximizes structural efficiency, and ensures mission-specific performance constraints are satisfied through the optimal design of load-bearing configurations, materials, and geometries in spacecraft structures.
79
Publications
2.6K
Citations
194
Authors
87
Institutions
Publications per year
2017–2026
9
Parents
79
1–5 of 79
194
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87

Langley Research Center
Hampton, United States
8 h-index
12 publications
218 citations
Lockheed Martin (United States)
Bethesda, United States
4 h-index
5 publications
99 citations
China Academy of Space Technology
Beijing, China
4 h-index
8 publications
288 citations

Howard University
Washington, United States
3 h-index
4 publications
48 citations
University of Illinois Urbana-Champaign
Urbana, United States
3 h-index
5 publications
611 citations

University of Pisa
Pisa, Italy
3 h-index
6 publications
202 citations
Purdue University West Lafayette
West Lafayette, United States
2 h-index
6 publications
267 citations

Instituto Nacional de Pesquisas Espaciais
São José dos Campos, Brazil
2 h-index
2 publications
24 citations
1–8 of 87
32 publications · 1.1K citations
22
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4 publications · 126 citations
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3 publications · 72 citations
3
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Repository · 3 publications · 37 citations
3
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3 publications · 212 citations
3
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1–5