This viewgraph presentation provides an overview of thermal-mechanical cyclic tests conducted on a composite cryogenic tank designed for reusable launch vehicles. Topics covered include: a structural analysis of the composite cryogenic tank, a description of Marshall Space Flight Center's Cryogenic Structure Test Facility, cyclic test plans and accomplishments, burst test and analysis and post-testing evaluation.


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    Titel :

    Thermal-Mechanical Cyclic Test of a Composite Cryogenic Tank for Reusable Launch Vehicles


    Beteiligte:
    Messinger, Ross (Autor:in) / Pulley, John (Autor:in)

    Kongress:

    44th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics, & Material Conference ; 2003 ; Norfolk, VA, United States


    Erscheinungsdatum :

    2003-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Thermal-Mechanical Cyclic Test of a Composite Cryogenic Tank for Reusable Launch Vehicles

    Messinger, R. / Pulley, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003



    Conformal Cryogenic Tank Trade Study for Reusable Launch Vehicles

    Rivers, H. K. / University of New Mexico; School of Engineering; Institute for Space and Nuclear Power Studies | British Library Conference Proceedings | 1999


    A CMC-Based Thermal Protection System for Cryogenic Tank Reusable Launch Vehicles

    Hald, H. et al. | British Library Conference Proceedings | 1998


    Feasibility Study of CFRP Application to the Cryogenic Propellant Tank of Reusable Launch Vehicles

    Shimoda, T. / Morino, Y. / Morimoto, T. | British Library Conference Proceedings | 2000