Flight Envelope Analysis

Flight Envelope Analysis is a systematic methodological framework in missile flight dynamics that characterizes the operational limits of a missile’s achievable flight conditions by defining the boundaries of its aerodynamic, propulsive, and structural performance under varying atmospheric and kinematic constraints.

310

Publications

8K

Citations

791

Authors

222

Institutions

Publications per year

2017–2026

60

Authors

791

  1. HM
    Hever Moncayo

    West Virginia University, United States

    6 publications · 209 citations

    6

    h-index

  2. MP
    Mario Perhinschi

    West Virginia University, United States

    6 publications · 209 citations

    6

    h-index

  3. JD
    Jennifer Davis

    West Virginia University, United States

    6 publications · 209 citations

    6

    h-index

  4. CC
    Coen C. de Visser

    Delft University of Technology, Netherlands

    6 publications · 145 citations

    6

    h-index

  5. SP
    Shripad P. Mahulikar

    Indian Institute of Technology Bombay, India

    5 publications · 256 citations

    5

    h-index

1–5 of 791

Venues

  1. Journal of Spacecraft and Rockets

    38 publications · 715 citations

    17

    h-index

  2. Journal of Guidance Control and Dynamics

    21 publications · 926 citations

    16

    h-index

  3. Journal of Aircraft

    21 publications · 539 citations

    15

    h-index

  4. Aerospace Science and Technology

    AST · 17 publications · 561 citations

    14

    h-index

  5. NASA Technical Reports Server (NASA)

    Repository · 7 publications · 119 citations

    7

    h-index

1–5