Spacecraft Structural Loads
Spacecraft Structural Loads is the singular academic construct denoting the quantified external and internal forces, moments, pressures, and accelerations imposed on a spacecraft's structure during launch, orbital operations, and re-entry, distinguished by their dynamic nature and mission-specific variability.
25
Publications
692
Citations
86
Authors
23
Institutions
Publications per year
2017–2026
2
Parents
25
C-5A Active Load Alleviation System
Tom Disney · Journal of Spacecraft and Rockets · 1977 · 37 citations
1–5 of 25
86
3
h-index
European Space Research and Technology Centre, Netherlands
2 publications · 67 citations
2
h-index
1
h-index
1 publications · 21 citations
1
h-index
1 publications · 21 citations
1
h-index
1–5 of 86
23
Marshall Space Flight Center
Redstone Arsenal, United States
3 h-index
5 publications
99 citations

Langley Research Center
Hampton, United States
2 h-index
3 publications
65 citations
Lockheed Martin (Canada)
Ottawa, Canada
2 h-index
4 publications
74 citations

European Space Research and Technology Centre
Noordwijk-Binnen, The Netherlands
2 h-index
4 publications
183 citations
L.Garde (United States)
Tustin, United States
1 h-index
2 publications
38 citations
Analytical Mechanics Associates (United States)
Hampton, United States
1 h-index
1 publications
22 citations

Baltic State Technical University Voenmeh
St Petersburg, Russia
1 h-index
1 publications
20 citations
Massachusetts Institute of Technology
Cambridge, United States
1 h-index
1 publications
13 citations
1–8 of 23
4 publications · 89 citations
4
h-index
2 publications · 91 citations
2
h-index
1 publications · 19 citations
1
h-index
1 publications · 10 citations
1
h-index
1 publications · 20 citations
1
h-index
1–5