Launch Mass Analysis
Launch Mass Analysis is a methodological framework within the field of mass properties engineering that systematically evaluates the total mass and its distribution characteristics of a spacecraft or launch vehicle during the design and pre-launch phases to ensure compliance with performance, stability, and mission constraints.
30
Publications
846
Citations
72
Authors
28
Institutions
Publications per year
2017–2026
5
Parents
30
Magnetic ZEKE experiments with mass analysis
Géza I. Németh, H. L. Selzle, E. W. Schlag · Chemical Physics Letters · 1993 · 133 citations · Full text
Traveling-wave induction launchers
D. G. Elliott · IEEE Transactions on Magnetics · 1989 · 39 citations
1–5 of 30
72
3
h-index
1
h-index
1
h-index
1
h-index
1
h-index
1–5 of 72
28

University of Strathclyde
Glasgow, United Kingdom
2 h-index
3 publications
55 citations

University of Glasgow
Glasgow, United Kingdom
2 h-index
4 publications
84 citations
Jet Propulsion Laboratory
Pasadena, United States
2 h-index
2 publications
53 citations

Glenn Research Center
Cleveland, United States
2 h-index
3 publications
85 citations
Johnson Space Center
Houston, United States
1 h-index
2 publications
40 citations
Nanjing University of Science and Technology
Nanjing, China
1 h-index
3 publications
78 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
1 h-index
3 publications
30 citations
Keldysh Institute of Applied Mathematics
Moscow, Russia
1 h-index
1 publications
15 citations
1–8 of 28
4 publications · 105 citations
4
h-index
2 publications · 44 citations
2
h-index
1 publications · 47 citations
1
h-index
1 publications · 11 citations
1
h-index
1 publications · 19 citations
1
h-index
1–5