Campo DC | Valor | Idioma |
dc.contributor.author | Shynkarenko, Olexiy | - |
dc.contributor.author | Simone, Domenico | - |
dc.date.accessioned | 2022-06-01T15:43:15Z | - |
dc.date.available | 2022-06-01T15:43:15Z | - |
dc.date.issued | 2020-08-07 | - |
dc.identifier.citation | SHYNKARENKO, Olexiy; SIMONE, Domenico. Oxygen?: methane torch ignition system for aerospace applications. Aerospace, v. 7, n. 8, 114, 2020. DOI: https://doi.org/10.3390/aerospace7080114. Disponível em: https://www.mdpi.com/2226-4310/7/8/114. Acesso em: 01 jun. 2022. | pt_BR |
dc.identifier.uri | https://repositorio.unb.br/handle/10482/43859 | - |
dc.language.iso | Inglês | pt_BR |
dc.publisher | MDPI | pt_BR |
dc.rights | Acesso Aberto | pt_BR |
dc.title | Oxygen-methane torch ignition system for aerospace applications | pt_BR |
dc.type | Artigo | pt_BR |
dc.subject.keyword | Sistema de ignição | pt_BR |
dc.subject.keyword | Maçarico a gás | pt_BR |
dc.subject.keyword | Combustão de metano-oxigênio | pt_BR |
dc.subject.keyword | Câmara de combustão | pt_BR |
dc.subject.keyword | Motores de foguetes | pt_BR |
dc.rights.license | c 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). | pt_BR |
dc.identifier.doi | https://doi.org/10.3390/aerospace7080114 | pt_BR |
dc.description.abstract1 | A new ignition system, based on a CH4/O2 torch has been developed by the Chemical Propulsion Laboratory of the University of Brasilia. Designed to ignite a hybrid rocket, this device has been improved to be used in testing of solid and liquid ramjet engines under development in our lab. The capability to provide multiple ignitions and to cool-down its combustion chamber walls by
using a swirled injection of the oxidizer, along with a very low weight to power ratio, makes this device versatile. The igniter is controlled by a feedback system, developed by our group, which guarantees the possibility of operating in different design conditions enabling, therefore, complete integration with systems of different nature. The main characteristics of the igniter and the design solutions are presented including some considerations about the tests performed to evaluate the quality and performance of the ignition system. | pt_BR |
dc.identifier.orcid | https://orcid.org/ 0000-0002-2934-1795 | pt_BR |
dc.identifier.orcid | https://orcid.org/ 0000-0002-4105-6700 | pt_BR |
dc.description.unidade | Faculdade UnB Gama (FGA) | - |
Aparece nas coleções: | Artigos publicados em periódicos e afins
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