A series of pyrotechnic shock tests were conducted to evaluate several concepts of attenuating the shock generated by the pyrotechnically actuated nuts during Transtage separation on the Titan IIIC launch vehicle. An orifice installed between the pyrotechnic device and the separation mechanism piston reduced shock levels by approximately 40%. This volume contains the shock response spectra from each of the 15 accelerometers for all 51 test runs.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Titan IIIC Transtage/Stage II Separation-Shock Bench Test. Volume III


    Beteiligte:
    G. E. Reed (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    824 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Titan IIIC digital flight controls

    FREEMAN, N. / TEETS, P. | AIAA | 1969



    Observations of Titan IIIC Transtage Fragmentation Debris

    Cowardin, H. | British Library Conference Proceedings | 2014


    Development of the Titan III transtage ACS hydrazine monopropellant rocket engine modules

    MAYBEE, D. / MORRISEY, D. / SKARTVEDT, C. et al. | AIAA | 1969