Mars Descent

Mars Descent is a methodological framework within entry systems that specifies the processes and technologies employed to safely reduce the velocity of a spacecraft and achieve controlled surface landing on Mars.

575

Publications

22.6K

Citations

2K

Authors

471

Institutions

Publications per year

2017–2026

120

Authors

2K

  1. RW
    Richard W. Powell

    Langley Research Center, United States

    18 publications · 839 citations

    17

    h-index

  2. RD
    Robert D. Braun

    Georgia Institute of Technology, United States

    20 publications · 1.5K citations

    17

    h-index

  3. DW
    David W. Way

    Langley Research Center, United States

    20 publications · 917 citations

    16

    h-index

  4. AS
    Adam Steltzner

    Jet Propulsion Laboratory, United States

    12 publications · 654 citations

    12

    h-index

  5. DK
    D. Kipp

    Jet Propulsion Laboratory, United States

    12 publications · 872 citations

    12

    h-index

1–5 of 2K

Venues

  1. Journal of Spacecraft and Rockets

    51 publications · 2.5K citations

    26

    h-index

  2. Acta Astronautica

    43 publications · 1.1K citations

    21

    h-index

  3. Icarus

    21 publications · 1.3K citations

    16

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 23 publications · 537 citations

    15

    h-index

  5. Advances in Space Research

    20 publications · 615 citations

    15

    h-index

1–5