Eva Smeets added file Chapters/13a.Mission_Profile.tex  almost 9 years ago

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\chapter{Performance Analysis}  \label{cha:performance}  %Please do not forget to add new symbols to the nomenclature e.g.: \nomenclature{$t_{element}$}{Thickness coefficient of plate \nomunit{[$-$]}}  Since the design is set to meet or even beat the current RBAR aircraft it is important to analyze the race and set the standards the aircraft should meet, the RBAR manoeuvres are analysed in Section~\ref{sec:man_RBAR}. In Chapter~\ref{cha:market} the market analysis showed that the design could also focus on other aerobatic competitions other than the RBAR. Therefore also these manoeuvres are analysed in this chapter in Section~\ref{sec:man_others}.  \input{Chapters/13a.Mission_Profile.tex}  \input{Chapters/13b.Maneuvres}           

\section{Mission Profile}  From requirements ARA-PW-EST-007 and ARA-PW-EST-008 it is known that the aircraft shall be able to fly the race at full throttle for 3 minutes and at 50\% throttle for 30 minutes for take off, landing and flying to the race location. The complete mission profile is shown in Figure~\ref{fig:mission_profile}. In this figure the profile during the race is not specified, the manoeuvres during the race are explained in Section~\ref{sec:man_RBAR}. When the aircraft is not being used for racing but for other aerobatic competitions the race would be replaced with the manoeuvres of the aerobatic competition.  \begin{figure}[htbp]  \centering  \includegraphics[width = \textwidth]{Figures/Mission_Profile}  \caption{The mission profile of the E-SPARC aircraft}  \label{fig:mission_profile}  \end{figure}