This disclosure includes a hybrid magneto-active membrane, which can be used as part of a Magneto-active Propellant Management Device (MAPMD), to actively control free surface effects of liquid materials, such as fuels, and to reduce fuel slosh. The disclosed MAPMD merges aspects of a diaphragm membrane with a magneto-active inlay to control the membrane during in-flight conditions.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Hybrid Magneto-Active Propellant Management Device for Active Slosh Damping in Spacecraft


    Beteiligte:

    Erscheinungsdatum :

    14.07.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H01F MAGNETS , Magnete



    A Hybrid Magneto-active Propellant Management Device for Active Slosh Damping in Spacecraft

    Sivasubramanian, Balaji / Paul, Leander V. / Krishnappa, Sanjay et al. | AIAA | 2015


    Active Damping of Fuel Slosh Using a Hybrid Magneto-Active Propellant Management Device

    Paul, Leander V. / Sivasubramanian, Balaji / Putheenveed, Soumya D. et al. | AIAA | 2016


    A Hybrid Magnetostrictive Propellant Management Device for Active Slosh Damping in Spacecraft

    Sivasubramanian, Balaji / Paul, Leander V. / Krishnappa, Sanjay et al. | AIAA | 2015


    Hybrid magneto-active propellant management device for active slosh damping within a vehicle fuel tank

    SIVASUBRAMANIAN BALAJI / PAUL LEANDER / GANGADHARAN SATHYA | Europäisches Patentamt | 2018

    Freier Zugriff

    Active Damping of Fuel Slosh Using a Hybrid Magneto-Active Propellant Management Device (AIAA 2016-1595)

    Paul, Leander V. / Sivasubramanian, Balaji / Putheenveed, Soumya D. et al. | British Library Conference Proceedings | 2016