This is lecture to be given at the IPPW 2016, as part of the 2 day course on Short Course on Destination Venus: Science, Technology and Mission Architectures. The attached presentation material is intended to be introduction to entry aspects of Venus in-situ robotic missions. The presentation introduces the audience to the aerodynamic and aerothermodynamic aspects as well as the loads, both aero and thermal, generated during entry. The course touches upon the system design aspects such as TPS design and both high and low ballistic coefficient entry system concepts that allow the science payload to be protected from the extreme entry environment and yet meet the mission objectives.


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    Title :

    Entry at Venus


    Contributors:

    Conference:

    International Planetary Probe Workshop ; 2016 ; Laurel, MD, United States


    Publication date :

    2016-06-13


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Pioneer Venus entry simulator

    Johns, C. E. | NTRS | 1976


    ESA Venus Entry Probe Study

    vandenBerg, M. L. / Falkner, P. / Phipps, A. et al. | NTRS | 2005


    Simulation of Venus atmospheric entry by earth re-entry.

    SPIEGEL, J. M. / WOLF, F. / ZEH, D. W. | AIAA | 1969


    Simulation of Venus atmospheric entry by earth re-entry

    SPIEGEL, J. / WOLF, F. / ZEH, D. | AIAA | 1968


    Challenges of a Venus entry mission

    Sengupta, Anita / Hall, Leslie | IEEE | 2011