Spacecraft Structural Stability

Spacecraft Structural Stability is a structural performance attribute that denotes the capacity of a spacecraft's load-bearing system to maintain its intended geometric configuration and resist buckling, deformation, or collapse under static and dynamic mechanical, thermal, and inertial loads encountered during launch, orbital operations, and re-entry.

57

Publications

1.7K

Citations

135

Authors

61

Institutions

Publications per year

2017–2026

6

Authors

135

  1. SR
    S. Rubin

    The Aerospace Corporation, United States

    2 publications · 104 citations

    2

    h-index

  2. PG
    P. G. Fuechsel

    Johns Hopkins University Applied Physics Laboratory, United States

    2 publications · 49 citations

    2

    h-index

  3. MS
    M. S. Anderson

    Langley Research Center, United States

    2 publications · 50 citations

    2

    h-index

  4. PM
    Peter M. Bainum

    Howard University, United States

    2 publications · 49 citations

    2

    h-index

  5. DL
    D. L. Mingori

    University of California, Los Angeles, United States

    2 publications · 47 citations

    2

    h-index

1–5 of 135

Venues

  1. Journal of Spacecraft and Rockets

    24 publications · 660 citations

    15

    h-index

  2. Aerospace Science and Technology

    AST · 3 publications · 94 citations

    3

    h-index

  3. Acta Astronautica

    3 publications · 133 citations

    3

    h-index

  4. Journal of Guidance Control and Dynamics

    2 publications · 71 citations

    2

    h-index

  5. Dynamics Specialists Conference

    Conference · 1 publications · 11 citations

    1

    h-index

1–5