Aerocapture using a towed, inflatable ballute system has been shown to provide a sifnificatn performance advantages compared to traditional technologies, including lower heating rates and accomodation of larger navigational uncertainties. This paper extends previous results by designing a ballute aerocapture separation algorithm that can operate in a more realistic Titan atmospheric model based on TitanGRAM.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Titan ballute aerocapture using the stochastic TitanGRAM model


    Beteiligte:

    Kongress:

    AIAA/AAS Space Flight Mechanics Conference ; 2004 ; Maui, HI, United States


    Erscheinungsdatum :

    2004-02-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Titan Ballute Aerocapture Using a Perturbed TitanGRAM Model

    Johnson, Wyatt / Lyons, Dan | AIAA | 2004


    Ballute Aerocapture Trajectories at Titan (AAS 03-646)

    Lyons, D. T. / Johnson, W. / American Astronautical Society | British Library Conference Proceedings | 2004


    AIAA-2004-5280 Titan Ballute Aerocapture Using a Perturbed TitanGRAM Model

    Johnson, W. / Lyons, D. | British Library Conference Proceedings | 2004


    Aeroelastic Design Considerations of a Clamped Ballute for Titan Aerocapture

    Rohrschneider, Reuben / Braun, Robert | AIAA | 2007