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ASTRIUM - Index of

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Launch vehicle : trajectory overview<br />

<strong>ASTRIUM</strong><br />

• Find the optimum trajectory compliant with the<br />

mission and design constraints<br />

Orbit injection<br />

- position<br />

- velocity<br />

Fairing jettison<br />

(thermal flux)<br />

Thermal flux<br />

Stage separations<br />

(dynamic pressure)<br />

120km<br />

Stage fall-out<br />

Atmospheric phase<br />

- loads<br />

- control<br />

Launch pad<br />

visibility<br />

fragmentation<br />

station 1 station 2<br />

Close safety<br />

Far safety<br />

Debris impact zone<br />

Page 9<br />

Ce document et les informations qu'il contient sont propriété d'Astrium. Il ne doit pas être utilisé à d'autres fins que celles pour lesquelles il a été remis. Il ne peut être ni<br />

reproduit, ni divulgué à des tiers (en tout ou partie) sans l'accord préalable et écrit d'Astrium. Astrium SAS – Tous droits réservés. // This document and the information it<br />

contains are property <strong>of</strong> Astrium. It shall not be used for any purpose other than those for which it was supplied. It shall not be reproduced or disclosed (in whole or in part) to<br />

any third party without Astrium prior written consent. Astrium SAS – All rights reserved.

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