Igniter Design

Igniter Design is a specialized engineering methodology within solid rocket motor technology that specifies the structural, material, and energetic configurations necessary to initiate reliable and controlled combustion of the solid propellant grain.

119

Publications

3K

Citations

451

Authors

154

Institutions

Publications per year

2017–2026

37

Authors

451

  1. CN
    Carlo N. Grimaldi

    University of Perugia, Italy

    4 publications · 96 citations

    4

    h-index

  2. PR
    P. R. Smy

    University of Alberta, Canada

    4 publications · 114 citations

    4

    h-index

  3. YI
    Yuji Ikeda

    Imagineering (Japan), Japan

    4 publications · 96 citations

    4

    h-index

  4. ZZ
    Zhibo Zhang

    Air Force Engineering University, China

    4 publications · 95 citations

    4

    h-index

  5. RM
    R. M. Clements

    University of Victoria, Canada

    4 publications · 114 citations

    4

    h-index

1–5 of 451

Venues

  1. 11

    h-index

  2. Journal of Propulsion and Power

    8 publications · 283 citations

    8

    h-index

  3. Propellants Explosives Pyrotechnics

    7 publications · 139 citations

    7

    h-index

  4. Sensors and Actuators A Physical

    6 publications · 286 citations

    6

    h-index

  5. Combustion and Flame

    5 publications · 168 citations

    5

    h-index

1–5