Development and design of 2-ft diam cassegrain monopulse antenna assembly for Lunar Module Rendezvous Radar; radar will provide position and rate information on range and angles between Lunar Module and Command Service Module for navigation and guidance computations during lunar stay and ascent-rendezvous phases of Apollo Mission; controlling factors such as performance requirements, angular coverage, and envelope restrictions are discussed; principal design features are presented. (31001)


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    Titel :

    Tracking antenna for space rendezvous


    Weitere Titelangaben:

    ASME -- Aviation and Space -- Progress and Prospects


    Beteiligte:
    Carter, W.W. (Autor:in) / Harmening, W.A. (Autor:in)

    Kongress:

    ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Tracking



    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Cassegrainian monopulse tracking antenna for space rendezvous.

    Carter, W. W. / Powell, W. E. | NTRS | 1966



    Space Rendezvous

    NTIS | 1994


    Optical tracking for rendezvous

    Wyman, C. L. | NTRS | 1963


    Rendezvous in space

    Stehling, K.R. | Engineering Index Backfile | 1961