ASTRIUM - Index of
ASTRIUM - Index of
ASTRIUM - Index of
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Advanced projects – future launch<br />
vehicles<br />
Reusable launch vehicles<br />
– Same problem and solving process<br />
– More complex configuration definition (aerodynamic,<br />
atmospheric flight, angle <strong>of</strong> attack different from 0)<br />
<strong>ASTRIUM</strong><br />
Page 19<br />
– Additional recovery<br />
constraints<br />
– Example for a TSTO :<br />
Search <strong>of</strong> an optimization<br />
between the two stages.<br />
for both the Booster<br />
return to the launch site,<br />
including a cruise flight,<br />
and the Orbiter reentry,<br />
including the deorbitation<br />
maneuver<br />
Booster + Orbiter<br />
propelled<br />
1<br />
Kourou<br />
Booster<br />
ballistic<br />
Booster<br />
Air-breathed propelled<br />
Orbiter<br />
propelled<br />
~ 5-10 km<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.<br />
3<br />
2<br />
Booster<br />
gliding<br />
Ground<br />
LEO<br />
200 km
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