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Throttleable hybrid rocket engines for precise aerospace manoeuvres
 Kříž, Tomáš ; Šplíchal, Miroslav (referee) ; Mašek, Jakub (advisor)
Aim of this bachelor thesis is to describe current knowledge of hybrid rocket propulsion. Thesis describes the development of hybrid rocket engine, including its precise description of the engine. Afterwards there is chapter of important engine components, including the main requirements for these components. The distribution of fuels and oxidants is an essential part of the thesis, including a description of selected fuels and oxidants and their environmental burden. There is also comparison between these engines and commonly use ones, including its definitions. Last but not least, there is overview of companies that are dedicated to hybrid propulsion. Conclusion is devoted to the estimation of future development of hybrid propulsion.
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