System, developed by Giannini Controls Corp, to satisfy stringent requirements of space flights, consists of radioisotope source unit, radioisotope detector unit, computer-controller unit, and required output units such as display, telemetry, valve amplifiers, and valves; details of components; photographs of prototype installations and test results are presented to substantiate theoretical analyses for signal propagation and radiation pattern mapping including measurements under zero gravity conditions.


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    Titel :

    Nucleonic propellant gaging and utilization systems for space vehicles


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Wright, D.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Propellants



    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Nucleonic zero-g propellant gaging system

    Dyes, O. / Bupp, F.E. | Tema Archiv | 1976


    Propellant gaging and utilization for apollo spacecraft

    Ulicki, E. | Engineering Index Backfile | 1964


    Propellant Gaging and Utilization for the Apollo Spacecraft

    Ulicki, Edward | SAE Technical Papers | 1964


    Low-G Propellant Gaging

    G. Orton | NTIS | 1987