Spacecraft Reentry Dynamics
Spacecraft Reentry Dynamics is a theoretical framework within aerospace engineering that characterizes the motion, thermal, and aerodynamic behavior of a spacecraft as it transitions from exoatmospheric flight to atmospheric flight under the influence of gravity, drag, lift, and heating effects.
64
Publications
2.2K
Citations
167
Authors
65
Institutions
Publications per year
2017–2026
15
Parents
64
1–5 of 64
167
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65
Lockheed Martin (United States)
Bethesda, United States
3 h-index
6 publications
96 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
3 h-index
9 publications
280 citations

Langley Research Center
Hampton, United States
3 h-index
4 publications
162 citations
China Academy of Space Technology
Beijing, China
2 h-index
15 publications
248 citations

Samara National Research University
Samara, Russia
2 h-index
3 publications
78 citations
China Aerodynamics Research and Development Center
Mianyang, China
2 h-index
4 publications
277 citations
The Aerospace Corporation
El Segundo, United States
2 h-index
3 publications
124 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
2 h-index
10 publications
410 citations
1–8 of 65
7 publications · 204 citations
7
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Repository · 4 publications · 162 citations
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3 publications · 150 citations
4
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3 publications · 69 citations
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3 publications · 70 citations
3
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1–5