Astronomy & Astrophysics

All Figures

$\begin{figure} \par\includegraphics[width=15.9cm,clip]{INT76_Fig1.eps} \end{figure}$ Figure 1: The INTEGRAL-on-Proton launch and early orbit phase.
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In the text

$\begin{figure} \par\includegraphics[width=16cm,clip]{INT76_Fig2.eps} \end{figure}$ Figure 2: Overall launch window for INTEGRAL. Shading shows the areas of parameters forbidden due to ( $\times$ ) the solar aspect outside ( $50\hbox {$^\circ $ },\ 130\hbox {$^\circ $ }$ ) 7, 13 days after the lift-off, (/) the minimum height less than 7500 km, (|) the maximum eclipse duration larger than 1.7 h (countours of constant level are given also for 1.5 and 1.3 h), ( $\backslash$ ) the eclipse 10 min after the injection (dashed countours of constant level), dotted area is 10 min launch window determined by launcher.
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In the text

$\begin{figure} \par\includegraphics[width=16.8cm,clip]{INT76_Fig3.eps} \end{figure}$ Figure 3: Perigee height evolution for INTEGRAL.
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In the text

$\begin{figure} \par\includegraphics[width=15.9cm,clip]{INT76_Fig1.eps} \end{figure}$	Figure 1: The INTEGRAL-on-Proton launch and early orbit phase.
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$\begin{figure} \par\includegraphics[width=16.8cm,clip]{INT76_Fig3.eps} \end{figure}$	Figure 3: Perigee height evolution for INTEGRAL.
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