The Mars Exploration Rover (MER) mission utilizes the Mars Pathfinder (MPF) parachute design. The MPF parachute drag coefficient is a driver for the MER entry, descent, and landing (EDL) design. As a result, a good estimate of the performance of the MPF parachute at Mars is required.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Re-examination of Mars Pathfinder parachute drag coefficient estimate


    Beteiligte:
    Desai, P. (Autor:in) / Schofield, T. (Autor:in) / Lisano, M. (Autor:in)

    Kongress:

    17th Aerodynamic Decelerator Systems Conference


    Erscheinungsdatum :

    19.05.2003


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flight Reconstruction of the Mars Pathfinder Disk-Gap-Band Parachute Drag Coefficient

    Desai, Prasun / Schofield, John / Lisano, Mike | AIAA | 2003



    Flight Reconstruction of the Mars Pathfinder Disk-Gap-Band Parachute Drag Coefficient

    Desai, Prasun / Schofield, John T. / Lisano, Michael E. | NTRS | 2003


    Mars Pathfinder Parachute System Performance

    Witkowski, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1999


    Mars Pathfinder parachute system performance

    Witkowski, Allen | AIAA | 1999