Background and objectives of US Air Force Advanced Ballistic Re-Entry Systems (ABRES)/Atlas program; Atlas boosters can be provided for low modification and launch service cost; they are equipped with all-inertial guidance systems; radio-inertial guidance may be installed to replace former; Atlas Series E/F boosters are programmed and scheduled to boost hypersonic glide vehicles with injection at altitudes of 25,000 ft at over 20,000 fps, to place various payloads into low-altitude circular orbits up to 150 nautical mi, or, by use of small solid motors and implementing Hohmann transfer, entire tank with 2000-lb payload can be placed into 300-nautical mi circular orbit.


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    Titel :

    Atlas E/F launch vehicle research and development capabilities


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:

    Kongress:

    SAE Meeting ; 1966 Boosters



    Erscheinungsdatum :

    1966


    Format / Umfang :

    19 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Atlas E/F Launch Vehicle Research and Development Capabilities

    Kalogeris, John G. | SAE Technical Papers | 1966


    Lockheed Launch Vehicle: Status, Capabilities, and Plans for Development

    Cobb, J. L. / Davis, D. E. / AIAA | British Library Conference Proceedings | 1994


    Lockheed Launch Vehicle: Status, Capabilities, and Plans for Development

    Cobb, J. L. / Davis, D. E. / AIAA | British Library Conference Proceedings | 1994