Return Trajectory Design
Return Trajectory Design is a spacecraft trajectory design methodology that specifically governs the formulation and optimization of flight paths enabling a vehicle to travel from an interplanetary destination or orbital location back to Earth or another designated return point, distinguished from other trajectory designs by its focus on reversal of mission phase, re-entry conditions, and Earth-centered impact or capture constraints.
30
Publications
734
Citations
90
Authors
40
Institutions
Publications per year
2017–2026
4
Parents
30
Feasibility analysis for a manned mars free-return mission in 2018
Dennis A. Tito, Grant Anderson, J. P. Carrico et al. · 2013 · 36 citations
1–5 of 30
90
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United States Air Force Research Laboratory, United States
2 publications · 31 citations
2
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2
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1–5 of 90
40

National University of Defense Technology
Changsha, China
3 h-index
10 publications
204 citations
Tsinghua University
Beijing, China
2 h-index
6 publications
99 citations
Marshall Space Flight Center
Redstone Arsenal, United States
2 h-index
4 publications
235 citations
The University of Texas at Austin
Austin, United States
2 h-index
5 publications
107 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
2 h-index
2 publications
31 citations
University of Stuttgart
Stuttgart, Germany
2 h-index
5 publications
138 citations

Samara National Research University
Samara, Russia
2 h-index
3 publications
80 citations
Analytical Services
Falls Church, United States
1 h-index
2 publications
80 citations
1–8 of 40
7 publications · 164 citations
7
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4 publications · 162 citations
4
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2 publications · 77 citations
2
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2 publications · 43 citations
2
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AST · 2 publications · 58 citations
2
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1–5