AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312

AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312

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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Bibliographic Details
Main Authors: Pedro Luiz Kaled Da Cás, Cristiano Queiroz Vilanova, Manuel Nascimento Dias Barcelos Jr., Carlos Alberto Gurgel Veras
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2012-10-01
Series:Journal of Aerospace Technology and Management
Subjects:
Hybrid rocket propulsion
Multiphysics analysis
Design optimization.
Online Access:https://www.jatm.com.br/jatm/article/view/173

Internet

https://www.jatm.com.br/jatm/article/view/173

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