This autonomous experiment for foaming metals in space involved: (1) payload support structure; (2) furnace and foaming apparatus; (3) electronic controls; (4) battery power; and (5) metallurgy. Emphasis was laid on a modular design which was easily modifiable and which offered maximum durability, safety, and failure tolerance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Ultralight reactive metal foams produced as structural shapes in space: System design


    Beteiligte:
    Cocks, F. H. (Autor:in) / Morrill, J. P. (Autor:in) / Feldman, M. R. (Autor:in)


    Erscheinungsdatum :

    1984-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Structural Design Considerations for Ultralight Aircraft

    Johnson, David B. / Baughn, Terry V. | SAE Technical Papers | 1986


    Structural Design Considerations for Ultralight Aircraft

    Baughn,T.V. / Johnson,D.B. / Civil/Mechanical Engng.Dep.SMU,Dallas,US | Kraftfahrwesen | 1986


    Structural design considerations for ultralight aircraft

    Baughn, T.V. / Johnson, D.B. | Tema Archiv | 1986


    ULTRALIGHT DEPLOYABLE SPACE STRUCTURE PROTOTYPE

    Gdoutos, Eleftherios / Truong, Alan / Pedivellano, Antonio et al. | TIBKAT | 2020