Thermodynamic Vent System (TVS) and Multilayer Insulation (MLI) technology, originally developed for long term storage of cryogen propellants in microgravity, is ideally suited for propellant storage and delivery systems for solar thermal propulsion. With this technology the heat-induced pressure rise in the tank provides the propellant delivery pressure without the need for an auxiliary pressurant system, and propellant delivery is used to remove the excess heat to control tank pressure. The factors to consider in designing such a balanced system, are presented. An example of a minimum system design is presented along with examples of laboratory-tested hardware.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design Factors for Applying Cryogen Storage and Delivery Technology to Solar Thermal Propulsion


    Beteiligte:

    Kongress:

    Space Technology and Applications International Forum ; 1997 ; Albuquerque, NM, United States


    Erscheinungsdatum :

    10.12.1996


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Design Factors for Applying Cryogen Storage and Delivery Technology to Solar Thermal Propulsion

    Millis, M. G. / University of New Mexico; School of Engineering; Institute for Space and Nuclear Power Studies | British Library Conference Proceedings | 1997



    Aircraft propulsion incorporating a cryogen

    SIMON TAYLOR | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft Propulsion System Incorporating with Cryogen

    SIMON TAYLOR | Europäisches Patentamt | 2022

    Freier Zugriff

    Passive cryogen storage system

    MUSTAFI SHOUVANIK / FRANCOM MATTHEW / LI XIAOYI et al. | Europäisches Patentamt | 2022

    Freier Zugriff