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
Parents
119
A MEMS-based solid propellant microthruster with Au/Ti igniter
Kaili Zhang, S.K. Chou, Simon S. Ang et al. · Sensors and Actuators A Physical · 2005 · 142 citations
Engineering, Aerospace Engineering, Mechanical Engineering +12
Plasma torch igniter for scramjets
Timothy C. Wagner, Walter F. O’Brien, G. B. Northam et al. · Journal of Propulsion and Power · 1989 · 95 citations
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154
Nanjing University of Science and Technology
Nanjing, China
8 h-index
35 publications
838 citations

Xi'an Jiaotong University
Xi'an, China
4 h-index
5 publications
127 citations

University of Victoria
Victoria, Canada
4 h-index
4 publications
114 citations

University of Alberta
Edmonton, Canada
4 h-index
6 publications
197 citations
University of Perugia
Perugia, Italy
4 h-index
21 publications
515 citations

Centre National de la Recherche Scientifique
Paris, France
4 h-index
15 publications
684 citations
Air Force Engineering University
Xi'an, China
4 h-index
22 publications
497 citations
Imagineering (Japan)
Kobe, Japan
3 h-index
10 publications
261 citations
1–8 of 154
13 publications · 258 citations
11
h-index
8 publications · 283 citations
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7 publications · 139 citations
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6 publications · 286 citations
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5 publications · 168 citations
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