The Landing Parachute Demonstrator (LPD) was conceived as a low-cost, rapidly-developed means of providing soft landing for the Max Launch Abort System (MLAS) crew module (CM). Its experimental main parachute cluster deployment technique and off-the-shelf hardware necessitated a full-scale drop test prior to the MLAS mission in order to reduce overall mission risk. This test was successfully conducted at Wallops Flight Facility on March 6, 2009, with all vehicle and parachute systems functioning as planned. The results of the drop test successfully qualified the LPD system for the MLAS flight test. This document captures the design, concept of operations and results of the drop test.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Max Launch Abort System (MLAS) Landing Parachute Demonstrator (LPD) Drop Test


    Beteiligte:

    Erscheinungsdatum :

    01.05.2011


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    GN&C Design Overview and Flight Test Results from NASA's Max Launch Abort System (MLAS)

    Dennehy, Cornelius / Lanzi, Raymond / Ward, Philip | AIAA | 2010


    Air Data Boom System Development for the Max Launch Abort System (MLAS) Flight Experiment

    Woods-Vedeler, Jessica A. / Cox, Jeff / Bondurant, Robert et al. | NTRS | 2010


    GN&C Design Overview and Flight Test Results from NASA's Max Launch Abort System (MLAS)

    Dennehy, C. / Lanzi, R. / Ward, P. et al. | British Library Conference Proceedings | 2010


    GN and C Design Overview and Flight Test Results from NASA's Max Launch Abort System (MLAS)

    Dennehy, Cornelius J. / Lanzi, Ryamond J. / Ward, Philip R. | NTRS | 2010