Two-impulse Transfer Orbits
Two-Impulse Transfer Orbits is a spacecraft trajectory optimization method that belongs to the class of orbital transfer techniques and is distinguished by the application of exactly two instantaneous velocity impulses to achieve a fuel-efficient transition between two coplanar circular orbits.
24
Publications
592
Citations
33
Authors
23
Institutions
Publications per year
2017–2026
3
Parents
24
Optimum Orbital Transfer by Impulses
Lu Ting · ARS journal · 1960 · 41 citations
Natural Sciences, Aerospace Engineering, Celestial Mechanics +11
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33
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23
Federal Aviation Administration
Washington, United States
3 h-index
4 publications
88 citations
Jet Propulsion Laboratory
Pasadena, United States
2 h-index
4 publications
98 citations
Johnson Space Center
Houston, United States
2 h-index
2 publications
63 citations

Aston University
Birmingham, United Kingdom
2 h-index
2 publications
27 citations

Harbin Institute of Technology
Harbin, China
1 h-index
3 publications
42 citations
California Institute of Technology
Pasadena, United States
1 h-index
1 publications
32 citations
University of Alabama
Tuscaloosa, United States
1 h-index
1 publications
19 citations
Université de technologie de belfort-montbéliard
Belfort, France
1 h-index
1 publications
19 citations
1–8 of 23
9 publications · 255 citations
9
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5 publications · 98 citations
5
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2 publications · 60 citations
2
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1 publications · 46 citations
1
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1 publications · 14 citations
1
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1–5