Spacecraft Vibration Analysis
Spacecraft Vibration Analysis is a computational and experimental methodology within spacecraft structural engineering that characterizes dynamic responses of space vehicles to vibrational loads during launch and operational environments, distinguishing itself by its focus on predicting, mitigating, and validating structural integrity under time-varying inertial forces specific to aerospace missions.
163
Publications
5.2K
Citations
411
Authors
132
Institutions
Publications per year
2017–2026
35
Parents
163
Advances in spacecraft micro-vibration suppression methods
Xiaolei Jiao, Jinxiu Zhang, Wenbo Li et al. · Progress in Aerospace Sciences · 2023 · 147 citations
Engineering, Aerospace Engineering, Mechanical Engineering +12
Vibration Isolator for Large Space Telescopes
Allen J. Bronowicki · Journal of Spacecraft and Rockets · 2006 · 131 citations
1–5 of 163
411
7
h-index
4
h-index
4
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4
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4
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1–5 of 411
132

Harbin Institute of Technology
Harbin, China
16 h-index
47 publications
1.8K citations
Tsinghua University
Beijing, China
8 h-index
17 publications
354 citations
China Academy of Space Technology
Beijing, China
7 h-index
12 publications
388 citations

Langley Research Center
Hampton, United States
7 h-index
10 publications
256 citations

Beihang University
Beijing, China
7 h-index
10 publications
237 citations
Virginia Tech
Blacksburg, United States
6 h-index
13 publications
564 citations
Canadian Space Agency
Longueuil, Canada
5 h-index
9 publications
208 citations
University of California, Los Angeles
Los Angeles, United States
4 h-index
6 publications
216 citations
1–8 of 132
39 publications · 1.2K citations
19
h-index
15 publications · 918 citations
14
h-index
12 publications · 471 citations
12
h-index
11 publications · 440 citations
10
h-index
AST · 8 publications · 213 citations
8
h-index
1–5