It is known that highly-porous aluminum alloys and honeycomb structures are used as shock absorbers in landing devices and other elements of spacecraft. The paper presents the results of studies that allow us to estimate the mechanical properties and shock-absorbing characteristics of highly-porous aluminum alloys and honeycomb structures made of aluminum alloys with an initial average density of 190 to 2250 kg/m3. The basics to calculate the specific and effective energy of shock absorption are given. The model shock absorbers for the characteristic stages of the deformation diagrams are shown.


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    Titel :

    Application of highly-porous aluminum alloys and honeycomb structures in spacecraft landing devices


    Beteiligte:
    Popov, Yu.V. (Autor:in) / Markov, V. A. (Autor:in) / Pusev, V. I. (Autor:in) / Selivanov, V. V. (Autor:in) / Soloviev, Vladimir A. (Herausgeber:in) / Rogozin, Dmitry O (Herausgeber:in) / Aleksandrov, Anatoly A (Herausgeber:in) / Fedorov, Igor B (Herausgeber:in) / Mayorova, Vera I (Herausgeber:in)

    Kongress:

    XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION ; 2021 ; Moscow, Russia


    Erschienen in:

    Erscheinungsdatum :

    20.07.2023


    Format / Umfang :

    7 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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    R. Turner / G. L. Carr | NTIS | 1967


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    Kiker, John W. / Norman, Leland C. | SAE Technical Papers | 1967