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Predstavitev letala Cessna 206 v konfiguraciji za protitočno obrambo
ID Tabak, Žan Marko (Author), ID Mrlak, Tomaž (Mentor) More about this mentor... This link opens in a new window

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Abstract
V zadnjem času so vse bolj pogoste vremenske ujme, katere spremlja uničujoča toča z rušilnim vetrom in poplavami, zato je zračna protitočna obramba še toliko bolj pomembna. V svoji diplomski nalogi bom tako predstavil letalo Cessna TU206G, ki se v Letalskem centru Maribor uporablja za obrambo proti toči. Za ta tip letala je narejen izračun mase in ravnotežja, vzletno-pristajalnih zmogljivosti, zmogljivosti vzpenjanja ter preračun porabljenega časa, goriva in razdalje do zadane višine, za dve različni masi, v standardni in protitočni konfiguraciji. Predstavljena je dodatna oprema, ki je ključni del protitočnih operacij. Prikazane so zmogljivosti križarjenja pri različnih pogojih atmosfere ter primerjava pristajalne razdalje z vzletno pri maksimalni dovoljeni masi.

Language:Slovenian
Keywords:cessna 206, obramba proti toči, masa in ravnotežje, zmogljivosti, vzletna razdalja, hitrost vzpenjanja, pristajalna razdalja
Work type:Bachelor thesis/paper
Typology:2.11 - Undergraduate Thesis
Organization:FS - Faculty of Mechanical Engineering
Place of publishing:Ljubljana
Publisher:[Ž. M. Tabak]
Year:2023
Number of pages:XXII, 61 str.
PID:20.500.12556/RUL-148494 This link opens in a new window
UDC:629.7.016(043.2)
COBISS.SI-ID:183389699 This link opens in a new window
Publication date in RUL:25.08.2023
Views:3667
Downloads:82
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Secondary language

Language:English
Title:Presentation of the Cessna 206 aircraft in anti-hail fighting configuration
Abstract:
In recent times, there has been a notable increase in the frequency of extreme weather events, resulting in damage caused by hailstorms, floods, and destructive winds. Consequently, the significance of air anti-hail defense has grown significantly. In my diploma thesis I will explore the Cessna TU206G aircraft, used at the Maribor Aviation Center for hail defense. For this type of aircraft, the calculation of mass and balance, take-off and landing performance, climb performance and calculation of time, fuel and distance used to the desired height, for two different masses were made: one in standard configuration and the other in an anti-hail setup. This thesis also examines additional equipment that plays a pivotal role in anti-hail operations. Furthermore, the cruising performance of the aircraft in various atmospheric conditions is analyzed, and a comparison between the landing and takeoff distances at the maximum allowed mass is made.

Keywords:cessna 206, anti-hail operations, mass and balance, performance, takeoff distance, rate of climb, landing distance

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