Various components incorporated in system are divided into propellants, pressurization and expulsions system, engines and control; most types of propellants, available for attitude control systems and aspects of various pressurization schemes and their relation to overall-system are presented; highest efficiency in attitude control can only be realized by use of small rocket engines with either pulse, continuous or controlled thrust.


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    Titel :

    Chemical rocket engines and propulsion systems for attitude control and stabilization of space vehicles


    Weitere Titelangaben:

    Chemische Raketentriebwerke Fuer Lageregelungssysteme von Raumfahrzeugen


    Beteiligte:
    Cardullo, M.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Deutsch


    Schlagwörter :


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