Spacecraft Structural Optimization

Spacecraft Structural Optimization is a computational engineering methodology that systematically minimizes mass, maximizes structural efficiency, and ensures mission-specific performance constraints are satisfied through the optimal design of load-bearing configurations, materials, and geometries in spacecraft structures.

79

Publications

2.6K

Citations

194

Authors

87

Institutions

Publications per year

2017–2026

9

Authors

194

  1. RT
    Raphael T. Haftka

    University of Florida, United States

    4 publications · 89 citations

    4

    h-index

  2. AB
    Andrew Burns

    Lockheed Martin (Canada), Canada

    3 publications · 62 citations

    3

    h-index

  3. PM
    Peter M. Bainum

    Howard University, United States

    3 publications · 36 citations

    3

    h-index

  4. SM
    Suresh M. Joshi

    Langley Research Center, United States

    3 publications · 48 citations

    3

    h-index

  5. GM
    Giovanni Mengali

    University of Pisa, Italy

    3 publications · 101 citations

    3

    h-index

1–5 of 194

Venues

  1. Journal of Spacecraft and Rockets

    32 publications · 1.1K citations

    22

    h-index

  2. Structural and Multidisciplinary Optimization

    4 publications · 126 citations

    4

    h-index

  3. AIAA Journal

    3 publications · 72 citations

    3

    h-index

  4. NASA Technical Reports Server (NASA)

    Repository · 3 publications · 37 citations

    3

    h-index

  5. Journal of Guidance Control and Dynamics

    3 publications · 212 citations

    3

    h-index

1–5