Escape Trajectory Design
Escape Trajectory Design is a computational methodology in astrodynamics that determines the optimal path and propulsion requirements for a human-rated spacecraft to safely disengage from a gravitational body or hazardous environment during launch or orbital operations, distinguishing itself from general trajectory design by prioritizing crew safety, abort capability, and real-time adaptability under emergency conditions.
19
Publications
513
Citations
48
Authors
23
Institutions
Publications per year
2017–2026
3
19
Escape From a Circular Orbit Using Tangential Thrust
D. J. Benney · Jet propulsion · 1958 · 67 citations
1–5 of 19
48
CFD Research Corporation (United States), United States
1 publications · 12 citations
1
h-index
1
h-index
1
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1
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1
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1–5 of 48
23
Robert Bosch (Germany)
Stuttgart, Germany
2 h-index
4 publications
56 citations
Johnson Space Center
Houston, United States
2 h-index
4 publications
84 citations
Age UK
London, United Kingdom
2 h-index
2 publications
28 citations
University of Michigan
Ann Arbor, United States
1 h-index
2 publications
42 citations
Nanjing University
Nanjing, China
1 h-index
1 publications
12 citations

Langley Research Center
Hampton, United States
1 h-index
2 publications
48 citations
United Aircraft (Russia)
Moscow, Russia
1 h-index
1 publications
15 citations
Naval Air Warfare Center Training Systems Division
Orlando, United States
1 h-index
2 publications
24 citations
1–8 of 23
2 publications · 92 citations
2
h-index
1 publications · 15 citations
1
h-index
1 publications · 67 citations
1
h-index
1 publications · 12 citations
1
h-index
1 publications · 12 citations
1
h-index
1–5