Basic Considerations on Probes with Low Ballistic Coefficients

  • Hannes Griebel


To understand the technical concept behind an atmospheric sounding ballute for Mars, it is necessary to afford some attention to the peculiarities of such a configuration when it comes to atmospheric entry.


Aerodynamic Drag Service Module Entry Angle Mission Design Basic Consideration 
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Copyright information

© Vieweg+Teubner Verlag | Springer Fachmedien Wiesbaden GmbH 2011

Authors and Affiliations

  • Hannes Griebel

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