Návrh a realizácia experimentálneho hybridného raketového motora

Abstract

This article focuses on the design and construction of an experimental hybrid rocket engine with thrust control capability. The article further examines the methodological approaches that were used in the design and manufacture, in particular, the methods of analysis, synthesis and experimental verification of the proposed system. Using Autodesk Inventor and Fusion software, the process of 3D modelling of the individual engine components was carried out, from the initial designs to the final technical documentation. The practical part is devoted to the actual manufacturing and testing of the engine, describing the selection of materials, technological procedures, and compliance with safety measures. The main objective is to design and implement an experimental hybrid rocket engine with thrust control capability. The aim of the thesis has been fulfilled by the creation and successful testing of a working prototype of a hybrid rocket engine, which can be further used for teaching and furthertesting purposes.