Titan III space launching system consists of six building blocks, three-stage air-borne vehicle, two solid-propellant rocket motors, liquid-rocket engines for each core stage, guidance system, launch facility, and aerospace ground equipment; interfacing covers joining these blocks and their subsystems functionally; results of 3 yr of subsystem-interfacing experience on Titan III space launching system are presented.


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    Titel :

    Titan III interface program


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:
    Hibsman, D.E. (Autor:in) / Rector, R.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Titan IV Program

    NTIS | 1992


    Titan reliability program

    Thompson, F.A. / Stein, W.D. | Engineering Index Backfile | 1964


    The Titan Reliability Program

    Thompson, F. A. / Stein, W. D. | SAE Technical Papers | 1964


    Titan Launch Vehicle Program overview

    Frew, Jeffrey / Currier, Ian | AIAA | 1997


    The Evolution of the Titan Rocket-Titan I to Titan II

    Adams, L. J. / International Astronautical Federation / International Academy of Astronautics | British Library Conference Proceedings | 1997