Descent Systems

Descent Systems is a technical subsystem within spacecraft design that comprises the mechanisms and protocols enabling the controlled atmospheric entry and landing of a spacecraft, distinguished by its focus on trajectory regulation, thermal protection, and deceleration technologies.

448

Publications

17K

Citations

1.1K

Authors

298

Institutions

Publications per year

2017–2026

99

Authors

1.1K

  1. RD
    Robert D. Braun

    Georgia Institute of Technology, United States

    17 publications · 1.3K citations

    15

    h-index

  2. DW
    David W. Way

    Langley Research Center, United States

    15 publications · 798 citations

    14

    h-index

  3. BA
    Behçet Açıkmeşe

    University of Washington, United States

    15 publications · 1K citations

    14

    h-index

  4. RW
    Richard W. Powell

    Langley Research Center, United States

    13 publications · 679 citations

    13

    h-index

  5. PN
    Prasun N. Desai

    Langley Research Center, United States

    13 publications · 500 citations

    12

    h-index

1–5 of 1.1K

Venues

  1. Journal of Guidance Control and Dynamics

    41 publications · 2.4K citations

    26

    h-index

  2. Journal of Spacecraft and Rockets

    39 publications · 2.2K citations

    25

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 15 publications · 395 citations

    13

    h-index

  4. Acta Astronautica

    17 publications · 560 citations

    13

    h-index

  5. Aerospace Science and Technology

    AST · 13 publications · 276 citations

    12

    h-index

1–5