Spacecraft Structural Stability
Spacecraft Structural Stability is a structural performance attribute that denotes the capacity of a spacecraft's load-bearing system to maintain its intended geometric configuration and resist buckling, deformation, or collapse under static and dynamic mechanical, thermal, and inertial loads encountered during launch, orbital operations, and re-entry.
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1.7K
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135
Authors
61
Institutions
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2017–2026
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1–5 of 57
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Johns Hopkins University Applied Physics Laboratory, United States
2 publications · 49 citations
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Langley Research Center
Hampton, United States
7 h-index
13 publications
522 citations
Jet Propulsion Laboratory
Pasadena, United States
3 h-index
5 publications
140 citations
University of California, Los Angeles
Los Angeles, United States
3 h-index
5 publications
127 citations
The Aerospace Corporation
El Segundo, United States
2 h-index
4 publications
208 citations
Virginia Tech
Blacksburg, United States
2 h-index
4 publications
146 citations
University of Colorado Boulder
Boulder, United States
2 h-index
4 publications
74 citations
California Institute of Technology
Pasadena, United States
2 h-index
4 publications
73 citations
Goddard Space Flight Center
Greenbelt, United States
2 h-index
2 publications
25 citations
1–8 of 61
24 publications · 660 citations
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AST · 3 publications · 94 citations
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3 publications · 133 citations
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2 publications · 71 citations
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Conference · 1 publications · 11 citations
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