Spacecraft Structural Sizing

Spacecraft Structural Sizing is a methodological framework within spacecraft engineering that determines the optimal dimensions, configurations, and material specifications of load-bearing components to ensure structural integrity, mass efficiency, and mission compatibility under anticipated launch and in-orbit operational conditions.

28

Publications

797

Citations

83

Authors

35

Institutions

Publications per year

2017–2026

1

Authors

83

  1. LC
    Luca Cavagna

    Politecnico di Milano, Italy

    2 publications · 110 citations

    2

    h-index

  2. JH
    Joseph H. Saleh

    Georgia Institute of Technology, United States

    2 publications · 86 citations

    2

    h-index

  3. SR
    Sergio Ricci

    Politecnico di Milano, Italy

    2 publications · 110 citations

    2

    h-index

  4. LT
    Lorenzo Travaglini

    UNSW Sydney, Australia

    2 publications · 110 citations

    2

    h-index

  5. MS
    Martin Sippel

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

    2 publications · 24 citations

    2

    h-index

1–5 of 83

Venues

  1. Journal of Spacecraft and Rockets

    9 publications · 285 citations

    9

    h-index

  2. Acta Astronautica

    1 publications · 67 citations

    1

    h-index

  3. Advances in Space Research

    1 publications · 38 citations

    1

    h-index

  4. 1

    h-index

  5. Space Technology Conference and Exposition

    Conference · 1 publications · 10 citations

    1

    h-index

1–5