Landing tests made of 1/6-scale dynamic model to determine accelerations and motions for nominal flight paths of 60 and 90° (vertical), range of contact attitudes from -25 to 30°, and vertical velocity of 12.25 fps at contact; computations made by using Newton's second law of motion and force stroke characteristics of air bag to determine accelerations for flight path of 90° and contact attitude of 0°.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Landing characteristics of reentry capsule with torus-shaped air bag for load alleviation


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    McGehee, J.R. (Autor:in) / Hathaway, M.E. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Water-landing characteristics of reentry capsule

    McGhee, J.R. / Hathaway, M.E. / Vaughan, Jr., V.L. | Engineering Index Backfile | 1959



    Landing characteristics of lenticular-shaped reentry vehicle

    Blanchard, U.J. | Engineering Index Backfile | 1961