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

6

Authors

141

  1. CR
    Colin R. McInnes

    University of Strathclyde, United Kingdom

    3 publications · 111 citations

    3

    h-index

  2. KZ
    K. ZONDERVAN

    The Aerospace Corporation, United States

    2 publications · 47 citations

    2

    h-index

  3. LJ
    Les Johnson

    Marshall Space Flight Center, United States

    2 publications · 38 citations

    2

    h-index

  4. BG
    Brian Gilchrist

    University of Michigan, United States

    2 publications · 38 citations

    2

    h-index

  5. SW
    Seung Won Lee

    Soonchunhyang University, South Korea

    2 publications · 40 citations

    2

    h-index

1–5 of 141

Venues

  1. Journal of Spacecraft and Rockets

    11 publications · 699 citations

    10

    h-index

  2. Acta Astronautica

    3 publications · 82 citations

    3

    h-index

  3. 35th Joint Propulsion Conference and Exhibit

    Conference · 3 publications · 43 citations

    3

    h-index

  4. Journal of Guidance Control and Dynamics

    3 publications · 105 citations

    3

    h-index

  5. AIAA Journal

    2 publications · 32 citations

    2

    h-index

1–5