The ballute's purpose is to set the size and aerodynamic properties of the spacecraft, so that its entry trajectory and attitude along the flight path conform to mission requirements.


Stagnation Point Areal Density Martian Atmosphere Entry Angle Path Angle 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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© Vieweg+Teubner Verlag | Springer Fachmedien Wiesbaden GmbH 2011

Authors and Affiliations

  • Hannes Griebel

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