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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Titan III interface program


    Additional title:

    Astronautics Aeronautics


    Contributors:

    Published in:

    Publication date :

    1966


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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