Efficient method of pressurizing liquid rocket propellant tanks has been developed experimentally and demonstrated in full-scale, flight-weight ground test article employing storable propellants; system developed for pressurizing gas generation employs solid-stream reagent injection onto propellant surface by means of pulse-mode pressure control system; based on results of 100 tests at pressures to 200 psig, concept feasibility was established, negligible system vibration and propellant degradation were encountered, and moderate operating temperatures and reagent consumption were experienced.


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    Title :

    Chemical pressurization of hypergolic liquid propellants


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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