An optimized hybrid rocket motor for the SARA platform reentry system
This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the Brazilian recoverable satellite (SARA), which...
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Main Authors: | Cás, Pedro Luiz Kaled Da, Vilanova, Cristiano Queiroz, Barcelos Júnior, Manuel Nascimento Dias, Veras, Carlos Alberto Gurgel |
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Format: | Artigo |
Language: | English |
Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2017
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Subjects: | |
Online Access: |
http://repositorio.unb.br/handle/10482/28646 https://dx.doi.org/10.5028/jatm.2012.04032312 |
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