Double-Base Propellants is a type of solid rocket propellant composed primarily of a homogeneous mixture of nitrocellulose and nitroglycerin, distinguished from other solid propellants by its dual energetic components that each contribute both fuel and oxidizer functionalities within a single-phase matrix.
190
Publications
5.3K
Citations
468
Authors
125
Institutions
Publications per year
2017–2026
39
Parents
Publications
190
1–5 of 190
Authors
468
- NK
9
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8
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7
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6
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1–5 of 468
Institutions
125
Nanjing University of Science and Technology
Nanjing, China
14 h-index
80 publications
2.2K citations
High Energy Materials Research Laboratory
Pune, India
11 h-index
44 publications
930 citations
Beijing Institute of Technology
Beijing, China
8 h-index
32 publications
676 citations
National Defense Academy of Japan
Yokosuka, Japan
7 h-index
9 publications
221 citations
Princeton University
Princeton, United States
7 h-index
25 publications
1.5K citations
Polytechnic School of Algiers
Algiers, Algeria
7 h-index
26 publications
543 citations
Military Technical College
Cairo, Egypt
6 h-index
19 publications
779 citations
Pennsylvania State University
State College, United States
6 h-index
17 publications
672 citations
1–8 of 125
Venues
- AIAA Journal
22 publications · 948 citations
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- Propellants Explosives Pyrotechnics
29 publications · 604 citations
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- Journal of Propulsion and Power
12 publications · 479 citations
12
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- Combustion and Flame
9 publications · 228 citations
9
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- Symposium (International) on Combustion
7 publications · 113 citations
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