Thrust Available is the maximum thrust that an aircraft propulsion system is capable of producing at a given altitude, speed, and atmospheric condition, serving as a key performance parameter in the analysis of steady flight and climb capabilities.
14
Publications
373
Citations
38
Authors
13
Institutions
Publications per year
2017–2026
2
Parents
Publications
14
High Performance Green Propellant for Satellite Applications
Kjell Anflo, R. Möllerberg, Kenzo Neff et al. · 2009 · 21 citations
1–5 of 14
Authors
38
- DL
1
h-index
- AA
1
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- PP
1
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- DP
1
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- JS
1
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1–5 of 38
Institutions
13
University of Pisa
Pisa, Italy
2 h-index
3 publications
203 citations
Busek (United States)
Natick, United States
2 h-index
4 publications
74 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
1 h-index
1 publications
25 citations
University of Padua
Padua, Italy
1 h-index
2 publications
38 citations
Technion – Israel Institute of Technology
Haifa, Israel
1 h-index
2 publications
174 citations
Rockwell Automation (United States)
Milwaukee, United States
1 h-index
1 publications
16 citations
Moog (United States)
East Aurora, United States
1 h-index
2 publications
42 citations
University College London
London, United Kingdom
1 h-index
2 publications
24 citations
1–8 of 13
Venues
- Journal of Guidance Control and Dynamics
2 publications · 106 citations
2
h-index
- 24th AIAA International Communications Satellite Systems Conference
Conference · 1 publications · 12 citations
1
h-index
- Acta Astronautica
1 publications · 19 citations
1
h-index
- Journal of Fluid Mechanics
1 publications · 87 citations
1
h-index
- Journal of Propulsion and Power
2 publications · 31 citations
1
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1–5