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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    Titel :

    Titan III standardized space launch system


    Weitere Titelangaben:

    AIAA -- Tech Papers


    Beteiligte:

    Kongress:

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



    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    THE TITAN III STANDARDIZED SPACE LAUNCH SYSTEM

    BLEYMAIER, JOSEPH | AIAA | 1963


    TITAN 3 AND TITAN 4 SPACE LAUNCH VEHICLES

    Richards, G.R. | Online Contents | 1993


    Titan II planetary delivery launch system

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



    Titan Launch Vehicle Program overview

    Frew, Jeffrey / Currier, Ian | AIAA | 1997