Sandia laboratories has developed a parachute system which allows delivery of a payload from high speed and very low altitude while providing an acceptable low impact velocity. A hybrid computer simulation of the parachute delivery system is described. (ERA citation 03:033661)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hybrid Trajectory Simulation of a Parachute System


    Beteiligte:
    W. R. Bolton (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Parachute-Payload System Flight Dynamics and Trajectory Simulation

    Giorgio Guglieri | DOAJ | 2012

    Freier Zugriff

    UAV Parachute Deployment Trajectory

    Jayaraman, J. / Lurdharaj, A. / Dhandapani, P. | British Library Conference Proceedings | 1999


    Simulation of Motion Trajectory of Parachute Inflation Process

    Tian, Jia Lin ;He, Yun ;Chen, Lei | Trans Tech Publications | 2014


    A Hybrid Parachute Simulation Environment for the Orion Parachute Development Project

    Moore, J. / Morris, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011