AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312
Journal of Aerospace Technology and Management, 2012 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
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Academia EngineeringThe ordinary combination of the transport approximation for the scattering phase function with differential models for radiative and combined heat transfer in scattering media characterized by multiple scattering of thermal radiation has ...
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Model-Based Sequential Design of Experiments with Machine Learning for Aerospace Systems
AerospaceTraditional experimental design methods often face challenges in handling complex aerospace systems due to the high dimensionality and nonlinear behavior of such systems, resulting in nonoptimal experimental designs.
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