Interplanetary Escape Trajectories
Interplanetary Escape Trajectories is a specialized class of orbital trajectories defined within astrodynamics that enables a spacecraft to overcome the gravitational influence of a celestial body—typically a planet or moon—and transition into an interplanetary transfer path, distinguished by its specific energy, departure asymptote, and targeted hyperbolic excess velocity relative to the departure body.
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2017–2026
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Statistical Theory of Asteroid Escape Rates
Charles Jaffé, Shane D. Ross, Martin W. Lo et al. · Physical Review Letters · 2002 · 127 citations
Escape of asteroids from the main belt
Mikael Granvik, Alessandro Morbidelli, David Vokrouhlický et al. · Astronomy and Astrophysics · 2016 · 118 citations · Full text
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California Institute of Technology
Pasadena, United States
2 h-index
8 publications
845 citations
Jet Propulsion Laboratory
Pasadena, United States
2 h-index
6 publications
591 citations

Sapienza University of Rome
Rome, Italy
1 h-index
1 publications
34 citations

Glenn Research Center
Cleveland, United States
1 h-index
1 publications
10 citations
Observatoire de la Côte d’Azur
Nice, France
1 h-index
1 publications
118 citations

Delft University of Technology
Delft, The Netherlands
1 h-index
1 publications
13 citations
Stanford Medicine
Stanford, United States
1 h-index
1 publications
19 citations

University of Helsinki
Helsinki, Finland
1 h-index
1 publications
118 citations
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3 publications · 117 citations
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1 publications · 37 citations
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1 publications · 13 citations
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PRL · 1 publications · 127 citations
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1 publications · 10 citations
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