The increased thrust, higher engine performance, and greater reliability requirements of the Titan IIIM engines for application to the Manned Orbital Laboratory Program necessitated extensive redesign of the thrust chamber assembly as well as other major components for the Stage I engine. The report encompasses the design and development of the combustion chamber. (Author)


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    Titel :

    Program Titan IIIM Standard Space Launch Vehicle Component Development Report for the Titan IIIM Stage I Combustion Chamber


    Beteiligte:
    W. J. Nord (Autor:in)

    Erscheinungsdatum :

    1969


    Format / Umfang :

    235 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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