Propellant Compatibility
Propellant Compatibility is a material-interaction criterion that distinguishes the degree to which a liquid rocket propellant can coexist with engine materials and components without inducing detrimental chemical or physical degradation under operational conditions.
33
Publications
798
Citations
127
Authors
37
Institutions
Publications per year
2017–2026
9
Parents
33
1–5 of 33
127
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37
Marshall Space Flight Center
Redstone Arsenal, United States
3 h-index
4 publications
53 citations
High Energy Materials Research Laboratory
Pune, India
3 h-index
13 publications
285 citations

Beijing Institute of Technology
Beijing, China
3 h-index
11 publications
196 citations
Microbiology Institute of Shaanxi
Xi'an, China
2 h-index
14 publications
273 citations
Nanjing University of Science and Technology
Nanjing, China
2 h-index
12 publications
220 citations
White Sands Test Facility
Las Cruces, United States
2 h-index
3 publications
37 citations
Polytechnic School of Algiers
Algiers, Algeria
2 h-index
10 publications
315 citations
Vikram Sarabhai Space Centre
Thiruvananthapuram, India
2 h-index
5 publications
123 citations
1–8 of 37
7 publications · 180 citations
7
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3 publications · 39 citations
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1 publications · 21 citations
1
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1 publications · 24 citations
1
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1 publications · 79 citations
1
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1–5