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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    Title :

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


    Additional title:

    Chemische Raketentriebwerke Fuer Lageregelungssysteme von Raumfahrzeugen


    Contributors:


    Publication date :

    1962


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


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