Reentry Trajectory Design

Reentry Trajectory Design is a specialized methodology within spacecraft trajectory design that determines the optimal path and control strategies for a vehicle transitioning from space or upper atmosphere into the denser layers of Earth’s atmosphere, distinguishing itself by addressing aerothermal loads, deceleration constraints, and precision landing requirements unique to atmospheric reentry.

44

Publications

1.5K

Citations

130

Authors

48

Institutions

Publications per year

2017–2026

12

Authors

130

  1. NF
    Nicolas Fezans

    Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany

    1 publications · 10 citations

    2

    h-index

  2. DA
    Daniel Alazard

    Office National d'Études et de Recherches Aérospatiales, France

    1 publications · 10 citations

    2

    h-index

  3. BC
    Benjamin Carpentier

    Office National d'Études et de Recherches Aérospatiales, France

    1 publications · 10 citations

    2

    h-index

  4. YZ
    Yang Zhao

    National University of Defense Technology, China

    2 publications · 35 citations

    2

    h-index

  5. NI
    Nicole Imbert

    Office National d'Études et de Recherches Aérospatiales, France

    1 publications · 10 citations

    2

    h-index

1–5 of 130

Venues

  1. Advances in Space Research

    3 publications · 70 citations

    3

    h-index

  2. Aerospace Science and Technology

    AST · 3 publications · 128 citations

    3

    h-index

  3. AIAA Guidance, Navigation, and Control Conference

    Conference · 2 publications · 30 citations

    3

    h-index

  4. Journal of Guidance Control and Dynamics

    2 publications · 137 citations

    2

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 2 publications · 31 citations

    2

    h-index

1–5