The Inflatable Reentry Vehicle Experiment II launched August 17, 2009, from NASA Wallops Flight Facility. The three mission objectives were to demonstrate inflation and re-entry survivability, assess the thermal and drag performance of the reentry vehicle, and to collect flight data for comparison with analysis and design techniques used in vehicle development. The flight was a complete success, with the re-entry vehicle separating cleanly from the launcher, inflating as planned, and demonstrating stable flight through reentry and descent while on-board systems telemetered video and flight performance data to the ground.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flight Performance of the Inflatable Reentry Vehicle Experiment II


    Beteiligte:

    Kongress:

    International Planetary Probe Workshop 2010 (IPPW-7) ; 2010 ; Barcelona, Spain, Spain


    Erscheinungsdatum :

    2010-06-14


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flight Performance of the Inflatable Reentry Vehicle Experiment 3

    Dillman, Robert / DiNonno, John / Bodkin, Richard et al. | NTRS | 2013


    Flight Performance of the Inflatable Reentry Vehicle Experiment 3

    R. Dillman / J. DiNonno / R. Bodkin et al. | NTIS | 2013



    Low-Density Aerodynamics for the Inflatable Reentry Vehicle Experiment

    James Moss / Christopher Glass / Brian Hollis et al. | AIAA | 2006


    Inflatable Reentry Technology

    Adami, M. / Hromadkova, A. / Giovangrossi, G. et al. | British Library Conference Proceedings | 2004