A technique for designing a low-RF reflectivity thermal blanket is presented. Multi-layer insulation (MLI) blankets are employed to stabilize the temperature on spacecraft unit but they can be responsible of passive intermodulation products and high-mutual coupling between antennas since they are realized with metallic materials. The possibility to replace the last inner layer of a MLI blanket with an ultra-thin absorbing layer made of high-impedance surface absorber is discussed.


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    Titel :

    Low RF reflectivity spacecraft thermal blanket by using high-impedance surface absorbers


    Beteiligte:


    Erscheinungsdatum :

    01.05.2012


    Format / Umfang :

    1204060 byte



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Low RF Reflectivity Spacecraft Thermal Blanket by Using High-Impedance Surface Absorbers

    Costa, F. / Monorchio, A. / Carrubba, E. et al. | British Library Conference Proceedings | 2012


    SPACECRAFT THERMAL BLANKET

    ARISTOV VASILIJ FEDOROVICH | Europäisches Patentamt | 2016

    Freier Zugriff