Orbital Transfer Orbits

Orbital Transfer Orbits is a conceptual framework in celestial mechanics that designates a minimally energetic trajectory enabling the repositioning of a spacecraft between two distinct Keplerian orbits through controlled impulsive maneuvers.

45

Publications

1K

Citations

96

Authors

41

Institutions

Publications per year

2017–2026

7

Authors

96

  1. RB
    R. Broucke

    The University of Texas at Austin, United States

    3 publications · 86 citations

    3

    h-index

  2. AF
    A. F. B. A. Prado

    Instituto Nacional de Pesquisas Espaciais, Brazil

    3 publications · 86 citations

    3

    h-index

  3. GA
    Geoffrey A. Landis

    Glenn Research Center, United States

    2 publications · 33 citations

    2

    h-index

  4. RS
    Ronald S. Cohen

    Stanford University, United States

    1 publications · 10 citations

    1

    h-index

  5. BL
    Byoung-Soo Lee

    Korea Institute of Industrial Technology, South Korea

    1 publications · 23 citations

    1

    h-index

1–5 of 96

Venues

  1. Journal of Guidance Control and Dynamics

    8 publications · 182 citations

    8

    h-index

  2. NASA Technical Reports Server (NASA)

    Repository · 3 publications · 36 citations

    3

    h-index

  3. Advances in Space Research

    2 publications · 28 citations

    2

    h-index

  4. Celestial Mechanics and Dynamical Astronomy

    2 publications · 27 citations

    2

    h-index

  5. Acta Astronautica

    2 publications · 38 citations

    2

    h-index

1–5