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Overview of the development of small and medium lauchers
Dítě, Radovan ; Petrásek, Miloslav (referee) ; Daněk, Vladimír (advisor)
This bachelor's thesis describes the development of small and medium vehicle launchers. The dissertation is divided into four main parts. The first part deals with basic principles of rocketry and types of rocket propulsion. The second chapter describes historical develop-ment of rocketry. The third part describes the development of small and medium vehicle launchers. And the last part is dedicated to the description of current states of small vehicle launchers.
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Overview of launchers for manned flights
Šurkala, Martin ; Daniel, Miloš (referee) ; Daněk, Vladimír (advisor)
This Bachelor’s dissertation describes the development of rocket technology from its beginnings to space flight. The first section describes the basic principles of reactive propulsion and gives a brief description of the development of the first rockets. The following chapter describes the formation of modern astronautics as presented by leading scientists who were active in rocket technology during the early 20th century. The next part is focused on the German rocket program, which builds on the space programs of the USA and USSR (Russia). The last section describes rockets used by Europe, China and the private company SpaceX. This dissertation no only includes carriers used in the past but also carriers which are currently preparing for their first trip.
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Stability and controllability of the Z-143 airplane with a more powerful engine
Kochtík, Martin ; Matějů, Jiří (referee) ; Daněk, Vladimír (advisor)
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane Z 143 with the power unit Lycoming AEIO-580-B1A. The first part of the text focuses on a general description of the aircraft, its geometric characteristics and calculation of mass and aerodynamic characteristics. In terms of flight performance there are compared the values for contemporary model and developmental aircraft with a more powerful engine. Another part of the work deals with the calculation of properties in terms of stability and manageability. In this section regards the determination of the results of the flight characteristics and their assessment of whether they comply. In the end I discuss the individual results and comment the possible recommendations on correction or improvement of these properties.
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Evaluation of the differences between JAR-FCL and PART-FCL for pilot licenses
Poloch, Gabriel ; Daněk, Vladimír (referee) ; Nastálek, Ondřej (advisor)
This final bachelor thesis maps, in the introductory section, the history of aviation from the legal viewpoint of regulations. It represents a regulations JAR-FCL, which are valid until now. Further it represents a regulation Part-FCL, which is part of the EU Regulation No 1178/2011. This regulation is currently in a transitional period and gradually replaces JAR-FCL. The main part of this thesis deals with the evaluation of differences between these regulations, particularly in the field of pilot licenses and structure of pilot training.
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Low Speed Operations
Glinz, Jan ; Daněk, Vladimír (referee) ; Šošovička, Róbert (advisor)
This thesis explains the problems of low speed operations. It aims at stall speed, calculating the stall speed and factors affecting the stall speed. One chapter is about stall warning and safety devices. Another chapter deals with influence of the low speed operations at airplane and the way to piloting it.
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An overview of atmospheric carriers for launching satellites into Earth's orbit
Bačová, Alena ; Petrásek, Miloslav (referee) ; Daněk, Vladimír (advisor)
This bachelor´s thesis is dealing with an overview of aircrafts designed as a launch platform for an air launch of satellite into the low Earth orbit. The thesis is divided into four main parts. The first part describes main principles of reaction engine and its two types of engines. The second part provides an overview of aircrafts as launch platform in the USA. The third part deals with these launch platforms in the former SSSR. The fourth part is devoted to aircrafts as launch platform in the Europe.
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Flight performance analysis of the airplane VUT 081 KONDOR
Kerndl, Jindřich ; Daněk, Vladimír (referee) ; Zikmund, Pavel (advisor)
The aim of this diploma thesis is to analyse flight performance of airplane VUT-081 Kondor. The first part focuses on determination and estimation of aerodynamic characteristics of the airplane. Based on this data flight performance was calculated and evaluated according to CS-ELSA. The last part is dedicated to comparison of flight performance of VUT-081 Kondor with other similar airplanes.
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