Orbit Transfer Design
Orbit Transfer Design is a systematic methodology within astrodynamics that specifies the optimal sequence and execution of propulsive maneuvers to transition a spacecraft from an initial orbit to a target orbit, distinguished by its focus on efficiency metrics such as fuel consumption, transfer time, and operational constraints.
54
Publications
1.7K
Citations
141
Authors
63
Institutions
Publications per year
2017–2026
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Jet Propulsion Laboratory
Pasadena, United States
3 h-index
8 publications
168 citations
The Aerospace Corporation
El Segundo, United States
3 h-index
7 publications
100 citations
Marshall Space Flight Center
Redstone Arsenal, United States
3 h-index
4 publications
111 citations

University of Glasgow
Glasgow, United Kingdom
3 h-index
3 publications
111 citations
University of Illinois Urbana-Champaign
Urbana, United States
2 h-index
2 publications
184 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
2 h-index
5 publications
202 citations
California Institute of Technology
Pasadena, United States
2 h-index
3 publications
66 citations

Harbin Institute of Technology
Harbin, China
2 h-index
4 publications
58 citations
1–8 of 63
11 publications · 699 citations
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3 publications · 82 citations
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Conference · 3 publications · 43 citations
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3 publications · 105 citations
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2 publications · 32 citations
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