Escape Trajectory Design

Escape Trajectory Design is a computational methodology in astrodynamics that determines the optimal path and propulsion requirements for a human-rated spacecraft to safely disengage from a gravitational body or hazardous environment during launch or orbital operations, distinguishing itself from general trajectory design by prioritizing crew safety, abort capability, and real-time adaptability under emergency conditions.

19

Publications

513

Citations

48

Authors

23

Institutions

Publications per year

2017–2026

3

Authors

48

  1. AP
    Andrzej Przekwas

    CFD Research Corporation (United States), United States

    1 publications · 12 citations

    1

    h-index

  2. JM
    Jennifer Madsen

    Lockheed Martin (Canada), Canada

    1 publications · 24 citations

    1

    h-index

  3. RR
    Robin R. Saudemont

    The University of Texas at Austin, United States

    1 publications · 48 citations

    1

    h-index

  4. AY
    Alex Yurchenko

    Georgia Institute of Technology, United States

    1 publications · 92 citations

    1

    h-index

  5. SN
    Syed Nasir Danial

    Memorial University of Newfoundland, Canada

    1 publications · 10 citations

    1

    h-index

1–5 of 48

Venues

  1. Journal of Guidance Control and Dynamics

    2 publications · 92 citations

    2

    h-index

  2. ARS journal

    1 publications · 15 citations

    1

    h-index

  3. Jet propulsion

    1 publications · 67 citations

    1

    h-index

  4. 1

    h-index

  5. 1

    h-index

1–5