Thrust Vectoring Nozzles

Thrust Vectoring Nozzle is a type of propulsion nozzle that mechanically alters the direction of thrust output by deflecting the exhaust jet, thereby enabling controlled maneuverability of aerospace vehicles without relying solely on aerodynamic control surfaces.

85

Publications

2.5K

Citations

166

Authors

59

Institutions

Publications per year

2017–2026

13

Variants

Thrust Vectoring Nozzle

Authors

166

  1. BL
    B. L. Berrier

    Langley Research Center, United States

    11 publications · 340 citations

    11

    h-index

  2. FJ
    F. J. Capone

    Langley Research Center, United States

    9 publications · 160 citations

    9

    h-index

  3. KD
    Karen Deere

    Langley Research Center, United States

    7 publications · 505 citations

    7

    h-index

  4. JD
    Jeffrey D. Flamm

    Langley Research Center, United States

    5 publications · 290 citations

    5

    h-index

  5. ML
    M. L. Mason

    Langley Research Center, United States

    5 publications · 167 citations

    5

    h-index

1–5 of 166

Venues

  1. NASA Technical Reports Server (NASA)

    Repository · 10 publications · 315 citations

    10

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  2. NASA STI Repository (National Aeronautics and Space Administration)

    Repository · 9 publications · 160 citations

    9

    h-index

  3. 5

    h-index

  4. 4

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  5. Journal of Aircraft

    4 publications · 61 citations

    4

    h-index

1–5