The aim of this paper is to analyze the aeroelastic processes  developed during the starting phase of a rocket engine via a coupling fluid/structure code. This analysis gives a better understanding of the behavior of the ...

The aim of this paper is to analyze the aeroelastic processes developed during the starting phase of a rocket engine via a coupling fluid/structure code. This analysis gives a better understanding of the behavior of the ...

This work is a first step in the understanding of the interaction process between internal shock waves and the flow transition inside of a rocket nozzle that develops during the engine start-up phase or when the nozzle is ...

The main objective of this research work was to obtain two formulations of ablative composites. These composites are also known as ablative structural composites, for applications in atmospherically severe conditions ...

Convergent-Divergent nozzles are essential parts in rocket propulsion systems, a lot has been developed over the study of these nozzles, however, those studies are focused on large systems. The goal of this study was the ...

The present work presents a proposal that involves reverse engineering of the current solid rocket engines developed by the Aeronautics and Space Institute (IAE), for the design of a Microsatellite Launch Vehicle (VLM). ...