Propellant Formulation
Propellant Formulation is a systematic composition of chemical constituents and additives engineered to generate controlled thrust through regulated decomposition, distinguished by its specific balance of fuel, oxidizer, binder, and performance-modifying agents tailored for application in metered-dose inhalers, solid rocket motors, or analogous propulsion systems.
362
Publications
11.7K
Citations
1.1K
Authors
259
Institutions
Publications per year
2017–2026
91
362
Recent advances in new oxidizers for solid rocket propulsion
Djalal Trache, Thomas M. Klapötke, Lotfi Maiz et al. · Green Chemistry · 2017 · 304 citations
Engineering, Aerospace Engineering, Chemical Engineering +17
Rachid Amrousse, Toshiyuki Katsumi, Nobuyuki Azuma et al. · Combustion and Flame · 2016 · 150 citations · Full text
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High Energy Materials Research Laboratory
Pune, India
22 h-index
194 publications
5K citations
Fraunhofer Institute for Chemical Technology
Karlsruhe, Germany
13 h-index
37 publications
1.8K citations
Nanjing University of Science and Technology
Nanjing, China
11 h-index
49 publications
1.6K citations
Purdue University West Lafayette
West Lafayette, United States
11 h-index
35 publications
2.1K citations
Politecnico di Milano
Milan, Italy
11 h-index
31 publications
1.6K citations
Vikram Sarabhai Space Centre
Thiruvananthapuram, India
9 h-index
30 publications
978 citations
Polytechnic School of Algiers
Algiers, Algeria
7 h-index
36 publications
770 citations

Beijing Institute of Technology
Beijing, China
6 h-index
27 publications
855 citations
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55 publications · 1.6K citations
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24 publications · 762 citations
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15 publications · 354 citations
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12 publications · 1K citations
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13 publications · 379 citations
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