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
Format: Artigo
Language: English
Published: Departamento de Ciência e Tecnologia Aeroespacial 2017
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Online Access: http://repositorio.unb.br/handle/10482/28646
https://dx.doi.org/10.5028/jatm.2012.04032312
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