Cargando…
Stabilized detonation for hypersonic propulsion
Future terrestrial and interplanetary travel will require high-speed flight and reentry in planetary atmospheres by way of robust, controllable means. This, in large part, hinges on having reliable propulsion systems for hypersonic and supersonic flight. Given the availability of fuels as propellant...
Autores principales: | Rosato, Daniel A., Thornton, Mason, Sosa, Jonathan, Bachman, Christian, Goodwin, Gabriel B., Ahmed, Kareem A. |
---|---|
Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
National Academy of Sciences
2021
|
Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8157988/ https://www.ncbi.nlm.nih.gov/pubmed/33972449 http://dx.doi.org/10.1073/pnas.2102244118 |
Ejemplares similares
-
Experimental validation of rotating detonation for rocket propulsion
por: Bennewitz, John W., et al.
Publicado: (2023) -
Advances in hypersonics: modeling hypersonic flows
por: Bertin, John, et al.
Publicado: (1992) -
Detonation Dynamics
por: Zhang, F
Publicado: (2012) -
Detonation of condensed explosives
por: Chéret, Roger
Publicado: (1993) -
Proceedings of the Workshop on Hypersonic Flows for Reentry Problems
por: Désidéri, Jean-Antoine, et al.
Publicado: (1991)