Restartability is the inherent capability of a liquid rocket engine to undergo multiple controlled ignition sequences during a single mission, distinguishing it from single-use propulsion systems by enabling in-flight re-ignition for mission flexibility, orbital insertion, or de-orbit maneuvers.
8
Publications
311
Citations
22
Authors
6
Institutions
Publications per year
2017–2026
1
Publications
8
Reducing recovery time in a small recursively restartable system
George Candea, James Cutler, Armando Fox et al. · 2003 · 68 citations · Full text
Designing for High Availability and Measurability
George Candea, Armando Fox · 2001 · 23 citations · Full text
J. R. Hulka, Jaden Forde, R. Werling et al. · 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 1998 · 16 citations
Engineering, Aerospace Engineering, Mechanical Engineering +16
1–5 of 8
Authors
22
- GC
3
h-index
- AF
3
h-index
- HS
1
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- JF
1
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- KA
1
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1–5 of 22
Institutions
6
Stanford University
Stanford, United States
3 h-index
10 publications
736 citations
Utah State University
Logan, United States
1 h-index
1 publications
13 citations
Chalmers University of Technology
Gothenburg, Sweden
1 h-index
3 publications
84 citations
Samara State Technical University
Samara, Russia
1 h-index
2 publications
32 citations
Omsk State Technical University
Omsk, Russia
1 h-index
3 publications
33 citations
University of Colorado Boulder
Boulder, United States
1 h-index
2 publications
22 citations
1–6 of 6
Venues
- 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conference · 1 publications · 16 citations
1
h-index
- Acta Astronautica
1 publications · 11 citations
1
h-index
- IEEE Transactions on Automation Science and Engineering
1 publications · 28 citations
1
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1–3