Effort was made to include as much engineering information on each component as possible, consistent with usefulness and catalog size limitations. The contents of this catalog contain components which were qualified for use with spacecraft monopropellant hydrazine and inert gas attitude control systems. Thrust ranges up to 44.5 N (10.0 lbf) for hydrazine and inert gas systems were considered. Additionally, some components qualified for uses other than spacecraft attitude control are included because they are suitable for use in attitude controls systems. (Author)


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    Title :

    Attitude Control Propulsion Components, Volume 1


    Publication date :

    1974


    Size :

    309 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English