Studies carried out for method of space vehicle attitude control using forces developed by hydrogen peroxide thrust chambers; propellant characteristics and physical properties of 90% H2O2; details of reaction control propulsion pressure-fed system wherein regulated helium pressure applied to positive expulsion monopropellant tank supplies H2O2 to thrust chambers, where rapid decomposition occurs; subsystems involved; 3 basic operating modes which employ each subsystem independently or in combination; results of program.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Mercury capsule reaction control propulsion system


    Weitere Titelangaben:

    Missiles Space


    Beteiligte:
    Zoeckler, D.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Mercury capsule and its flight systems

    Faget, M.A. / Piland, R.O. | Engineering Index Backfile | 1960


    Mercury capsule and its flight systems

    Faget, M.A. / Piland, R.O. | Engineering Index Backfile | 1960



    Electric Propulsion Mission to Mercury

    Kostantinov, M. / Fedotov, G. | British Library Online Contents | 1997