Spacecraft Structural Sizing
Spacecraft Structural Sizing is a methodological framework within spacecraft engineering that determines the optimal dimensions, configurations, and material specifications of load-bearing components to ensure structural integrity, mass efficiency, and mission compatibility under anticipated launch and in-orbit operational conditions.
28
Publications
797
Citations
83
Authors
35
Institutions
Publications per year
2017–2026
1
Parents
28
1–5 of 28
83
2
h-index
2
h-index
2
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2
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
2 publications · 24 citations
2
h-index
1–5 of 83
35

Langley Research Center
Hampton, United States
6 h-index
11 publications
203 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
5 publications
239 citations
Swedish Defence Research Agency
Stockholm, Sweden
2 h-index
2 publications
24 citations
Massachusetts Institute of Technology
Cambridge, United States
1 h-index
2 publications
70 citations
United States Air Force Academy
Colorado Springs, United States
1 h-index
1 publications
95 citations
Foster-Miller (United States)
Waltham, United States
1 h-index
1 publications
29 citations

Polytechnic University of Bari
Bari, Italy
1 h-index
1 publications
30 citations

Old Dominion University
Norfolk, United States
1 h-index
1 publications
11 citations
1–8 of 35
9 publications · 285 citations
9
h-index
1 publications · 67 citations
1
h-index
1 publications · 38 citations
1
h-index
1 publications · 13 citations
1
h-index
Conference · 1 publications · 10 citations
1
h-index
1–5