Concepedia

Launch Vehicle Compatibility

Launch Vehicle Compatibility is a design constraint that specifies the degree to which an interplanetary spacecraft conforms to the physical, operational, and performance requirements of a given launch vehicle to enable successful integration and deployment.

3

Publications

48

Citations

9

Authors

3

Institutions

Publications per year

2017–2026

0

Parents

Publications

3

1–3 of 3

Authors

9

  1. PB
    Peter Barros

    Georgia Institute of Technology, United States

    1 publications · 13 citations

    1

    h-index

  2. DN
    Dimitri N. Mavris

    Georgia Institute of Technology, United States

    1 publications · 13 citations

    1

    h-index

  3. CB
    Cecile Burg

    Georgia Institute of Technology, United States

    1 publications · 13 citations

    1

    h-index

  4. YG
    Yanping Guo

    Johns Hopkins University Applied Physics Laboratory, United States

    1 publications · 19 citations

    1

    h-index

  5. BG
    Brand Griffin

    Marshall Space Flight Center, United States

    1 publications · 16 citations

    1

    h-index

1–5 of 9

Institutions

3

  1. Georgia Institute of Technology

    Atlanta, United States

    1 h-index

    5 publications

    65 citations

  2. Marshall Space Flight Center

    Redstone Arsenal, United States

    1 h-index

    1 publications

    16 citations

  3. Johns Hopkins University

    Baltimore, United States

    1 h-index

    2 publications

    38 citations

1–3 of 3

Venues

  1. AIAA SPACE 2014 Conference and Exposition

    Conference · 1 publications · 16 citations

    1

    h-index

  2. AIAA/AAS Astrodynamics Specialist Conference and Exhibit

    Conference · 1 publications · 19 citations

    1

    h-index

1–2