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National Repository of Grey Literature 2 records found  Search took 0.00 seconds. 
Design of airconditioned chamber for stratospherical baloon
 Gedeon, Sebastián ; Spáčil, Tomáš (referee) ; Krejsa, Jiří (advisor)
The aim of this bachelor thesis is design of a heating chamber for a stratospheric balloon. The chamber's role is to preserve the load from the impact of the environment in which the baloon is going to be situated. The process of protection of the load is described in three steps. The first one is to characterize the flight dynamics which consits of the following: elevation time, descending time, maximal height reached, air characteristics changes depending on time. The second step deals with flight energetic balance. The total heat losses or the total heat increase of the chamber in different weather conditions have to be defined resutling from step one. The third step is to design the constructing or functional elements of the heated chamber, so that the chamber could overcome extreme conditions during the flight and to prevent the damage to the load. The energetic balance calculations are presented in the Microsoft Excel document. This document is free to read and can help with scientific construction projects.
Detailed record
Design of airconditioned chamber for stratospherical baloon
 Gedeon, Sebastián ; Spáčil, Tomáš (referee) ; Krejsa, Jiří (advisor)
The aim of this bachelor thesis is design of a heating chamber for a stratospheric balloon. The chamber's role is to preserve the load from the impact of the environment in which the baloon is going to be situated. The process of protection of the load is described in three steps. The first one is to characterize the flight dynamics which consits of the following: elevation time, descending time, maximal height reached, air characteristics changes depending on time. The second step deals with flight energetic balance. The total heat losses or the total heat increase of the chamber in different weather conditions have to be defined resutling from step one. The third step is to design the constructing or functional elements of the heated chamber, so that the chamber could overcome extreme conditions during the flight and to prevent the damage to the load. The energetic balance calculations are presented in the Microsoft Excel document. This document is free to read and can help with scientific construction projects.
Detailed record

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