Solid rocket propellant and rocket motor components were aged in a vented container on the interior of the LDEF. The results of aging IPSM-II/PAM-DII space motor components are presented. Ballistic and mechanical properties of the space aged main propellant, igniter propellant, and ignition system were compared with similar data from preflight and ground aged samples. Mechanical properties of the composite materials and bonded joints used in the motor case, insulation, liner, nozzle, exit cone, and skirt were similarly evaluated. The space aging results are compared to data collected in a ground based vacuum aging program on similar components.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space aging of solid rocket materials


    Beteiligte:
    Lester, Dean M. (Autor:in) / Jones, Leon L. (Autor:in) / Smalley, R. B., Jr. (Autor:in) / Ord, R. Neil (Autor:in)


    Erscheinungsdatum :

    1991-06-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space Aging of Solid Rocket Materials

    D. M. Lester / L. L. Jones / R. B. Smalley et al. | NTIS | 1992


    Space Aging of Solid Rocket Materials

    Dean M Lester / Leon L Jones / R B Smalley, Jr et al. | NTRS | 1992


    Space Aging of Solid Rocket Materials (P0005)

    Leon L. Jones / R. B. Smalley, Jr. | NTRS | 1984


    Space Aging of Solid Rocket Materials (Abstract Only)

    D. M. Lester / L. L. Jones / R. B. Smalley et al. | NTIS | 1991


    Space Shuttle solid rocket booster

    Hardy, G. B. | NTRS | 1979