A program was conducted to provide the technology base for the SS/RCS flight tankage. Through a combination of analysis, subscale testing and computer predictions, a surface tension acquisition/expulsion system design was developed for the Orbiter RCS application. A full-scale tank system was fabricated and ground verification testing was conducted. Cleaning, inspection, fill and drain, and one-g expulsion performance were demonstrated. Results show that the fine-mesh screen, compartmented tank system provides the performance, flexibility, reusability, and other characteristics required by the pulsing, high flowrate RCS. It provides the required expulsion under widely differing high-g boost abort and reentry vectors oriented 119 deg apart and during on-orbit operation under omnidirectional low-g conditions.


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    Titel :

    Surface tension propellant acquisition system technology for Space Shuttle reaction control tanks


    Beteiligte:
    Fester, D. A. (Autor:in) / Villars, A. J. (Autor:in) / Uney, P. E. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics and Society of Automotive Engineers, Propulsion Conference ; 1975 ; Anaheim, CA


    Erscheinungsdatum :

    01.09.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Surface Tension Propellant Acquisition System Technology for Space Shuttle Reaction Control Tanks

    Dale A. Fester / Ashton J. Villars / Preston E. Uney | AIAA | 1976


    Space Shuttle Reaction Control Subsystem Propellant Acquisition Technology

    Dale A. Fester / Ralph N. Eberhardt / James R. Tegart | AIAA | 1975


    Space Shuttle Reaction Control Subsystem propellant acquisition

    Fester, D. A. / Eberhardt, R. N. / Tegart, J. R. | NTRS | 1974


    Space Shuttle Reaction Control Subsystem propellant acquisition

    FESTER, D. / EBERHARDT, R. / TEGART, J. | AIAA | 1974