Launch Vehicle Integration

Launch Vehicle Integration is the process of aligning, adapting, and certifying a small satellite’s mechanical, electrical, thermal, and operational interfaces to meet the specific physical, environmental, and mission requirements of a launch vehicle, ensuring compatibility and safe deployment.

116

Publications

2.7K

Citations

466

Authors

95

Institutions

Publications per year

2017–2026

13

Authors

466

  1. JO
    John Olds

    Georgia Institute of Technology, United States

    6 publications · 168 citations

    5

    h-index

  2. DC
    D. C. Freeman

    Langley Research Center, United States

    3 publications · 97 citations

    3

    h-index

  3. RA
    Robert Austin

    North Carolina State University, United States

    3 publications · 97 citations

    3

    h-index

  4. HP
    H. Philip Stahl

    Marshall Space Flight Center, United States

    3 publications · 48 citations

    3

    h-index

  5. TA
    Theodore A. Talay

    Langley Research Center, United States

    3 publications · 97 citations

    3

    h-index

1–5 of 466

Venues

  1. Journal of Spacecraft and Rockets

    11 publications · 191 citations

    11

    h-index

  2. Acta Astronautica

    10 publications · 275 citations

    10

    h-index

  3. NASA Technical Reports Server (NASA)

    Repository · 7 publications · 123 citations

    7

    h-index

  4. Digital Commons - USU (Utah State University)

    Repository · 4 publications · 81 citations

    4

    h-index

  5. 4

    h-index

1–5