Concept of Titan III 624A Standard Space Launch System under development by U S Air Force Systems Command; its payload capability will range from 5000 to 25,000 lb and mission capability will include, low altitude elliptical orbit by direct injection, low altitude circular orbit, low altitude circular orbit with Hohmann transfer to another orbit, synchronous orbit, and deep space trajectory to escape; design approach and details of booster vehicle; concept of integrate-transfer-launch facility.


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    Title :

    Titan III standardized space launch system


    Additional title:

    AIAA -- Tech Papers


    Contributors:

    Conference:

    Meeting of the 2nd AIAA -- Manned Space Flight ; 1963 Launching



    Publication date :

    1963


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    THE TITAN III STANDARDIZED SPACE LAUNCH SYSTEM

    BLEYMAIER, JOSEPH | AIAA | 1963


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    Titan II planetary delivery launch system

    Howard, G. D. / McNamara, R. P. / International Academy of Astronautics | British Library Conference Proceedings | 1995