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.

10

Publications

456

Citations

22

Authors

16

Institutions

Publications per year

2017–2026

0

Authors

22

  1. GG
    G. Grimminger

    RAND Corporation, United States

    1 publications · 13 citations

    1

    h-index

  2. DF
    David Farrelly

    Utah State University, United States

    1 publications · 127 citations

    1

    h-index

  3. SD
    Shane D. Ross

    Virginia Tech, United States

    1 publications · 127 citations

    1

    h-index

  4. RH
    R. H. Stanford

    California Institute of Technology, United States

    1 publications · 70 citations

    1

    h-index

  5. LM
    L. M. Perko

    Northern Arizona University, United States

    1 publications · 19 citations

    1

    h-index

1–5 of 22

Venues

  1. Journal of Guidance Control and Dynamics

    3 publications · 117 citations

    3

    h-index

  2. Acta Astronautica

    1 publications · 37 citations

    1

    h-index

  3. Physics Today

    1 publications · 13 citations

    1

    h-index

  4. Physical Review Letters

    PRL · 1 publications · 127 citations

    1

    h-index

  5. AIP conference proceedings

    1 publications · 10 citations

    1

    h-index

1–5