Reentry Trajectory Design
Reentry Trajectory Design is a specialized methodology within spacecraft trajectory design that determines the optimal path and control strategies for a vehicle transitioning from space or upper atmosphere into the denser layers of Earth’s atmosphere, distinguishing itself by addressing aerothermal loads, deceleration constraints, and precision landing requirements unique to atmospheric reentry.
44
Publications
1.5K
Citations
130
Authors
48
Institutions
Publications per year
2017–2026
12
Parents
44
1–5 of 44
130
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
1 publications · 10 citations
2
h-index
Office National d'Études et de Recherches Aérospatiales, France
1 publications · 10 citations
2
h-index
Office National d'Études et de Recherches Aérospatiales, France
1 publications · 10 citations
2
h-index
2
h-index
Office National d'Études et de Recherches Aérospatiales, France
1 publications · 10 citations
2
h-index
1–5 of 130
48

Beihang University
Beijing, China
4 h-index
15 publications
515 citations

Northwestern Polytechnical University
Xi'an, China
3 h-index
7 publications
143 citations
China Academy of Launch Vehicle Technology
Beijing, China
3 h-index
3 publications
60 citations

Harbin Institute of Technology
Harbin, China
3 h-index
6 publications
140 citations
Beijing Aerospace Flight Control Center
Beijing, China
2 h-index
2 publications
74 citations

Beijing Institute of Technology
Beijing, China
2 h-index
4 publications
197 citations
Office National d'Études et de Recherches Aérospatiales
Palaiseau, France
2 h-index
1 publications
10 citations
Marshall Space Flight Center
Redstone Arsenal, United States
2 h-index
4 publications
327 citations
1–8 of 48
3 publications · 70 citations
3
h-index
AST · 3 publications · 128 citations
3
h-index
Conference · 2 publications · 30 citations
3
h-index
2 publications · 137 citations
2
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Repository · 2 publications · 31 citations
2
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1–5