NASA's planned advanced space transportation vehicles will benefit from the use of integral/conformal cryogenic propellant tanks which will reduce the launch weight and lower the earth-to-orbit costs considerably. To implement the novel concept of integral/conformal tanks requires developing an equally novel concept in thermal protection materials. Providing insulation against reentry heating and preserving propellant mass can no longer be considered separate problems to be handled by separate materials. A new family of materials, Superthermal Insulation (STI), has been conceiving and investigated by NASA's Ames Research Center to simultaneously provide both thermal protection and cryogenic insulation in a single, integral material.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Characterization of an Integral Thermal Protection and Cryogenic Insulation Material for Advanced Space Transportation Vehicles


    Beteiligte:

    Kongress:

    30th International Conference on Environmental Systems ; 2000 ; Toulouse, France


    Erscheinungsdatum :

    2000-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Reusable cryogenic foam insulation for advanced aerospace vehicles

    Mcauliffe, Patrick S. / Taylor, Allan H. / Sparks, Larry L. et al. | NTRS | 1991


    Reusable cryogenic foam insulation for advanced aerospace vehicles

    MCAULIFFE, PATRICK / TAYLOR, ALLAN / SPARKS, LARRY et al. | AIAA | 1991


    Shingle multilayer insulation for space vehicles using cryogenic fluids.

    Coston, R. M. / Elgin, D. R. / Parmley, R. T. | NTRS | 1966