Propulsion System Configuration
Propulsion System Configuration is a technical framework that specifies the arrangement, selection, and integration of propulsion components and subsystems within a spacecraft to achieve intended performance, mission objectives, and operational constraints.
145
Publications
4.1K
Citations
457
Authors
160
Institutions
Publications per year
2017–2026
40
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Glenn Research Center
Cleveland, United States
13 h-index
31 publications
863 citations

Langley Research Center
Hampton, United States
10 h-index
25 publications
683 citations
University of Michigan
Ann Arbor, United States
5 h-index
10 publications
304 citations

Ames Research Center
Mountain View, United States
4 h-index
4 publications
86 citations
Jet Propulsion Laboratory
Pasadena, United States
4 h-index
5 publications
94 citations
Marshall Space Flight Center
Redstone Arsenal, United States
4 h-index
10 publications
117 citations
Cranfield University
Cranfield, United Kingdom
3 h-index
12 publications
423 citations
HRL Laboratories (United States)
Malibu, United States
3 h-index
5 publications
61 citations
1–8 of 160
34 publications · 925 citations
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4 publications · 90 citations
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4 publications · 162 citations
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Repository · 3 publications · 51 citations
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3 publications · 187 citations
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