A test bed was fabricated under NASA/MSFC (National Aeronautics and Space Administration/Marshall Space Flight Center) Contract NAS8-36418 to demonstrate hydrogen/oxygen propulsion technology readiness for the initial operating condition (IOC) space station application. A water electrolysis module was later added to the initial test bed to simulate the baseline propulsion system configuration. This paper describes the activation and test results to date and presents plans for future testing.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space station propulsion system test bed and control system testing results


    Additional title:

    Pruefanlage fuer Raumstation-Antriebe und Ergebnisse der Pruefung der Regelsysteme


    Contributors:
    Norman, A.M. (author) / Briley, G.L. (author) / Nave, L.H. (author) / Pavlinsky, J.F. (author) / Allums, S. (author)

    Published in:

    AIAA-Papers ; Jul ; 1-11


    Publication date :

    1987


    Size :

    11 Seiten, 19 Bilder, 3 Tabellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Space Station propulsion system test bed and control system testing results

    NORMAN, A. / BRILEY, G. / NAVE, L. et al. | AIAA | 1987


    Space Station propulsion system test bed and control system testing results

    Norman, A. M. / Briley, G. L. / Nave, L. H. et al. | NTRS | 1987




    Space Station propulsion system test bed

    Norman, A. M. / Briley, G. L. / Evans, S. A. et al. | NTRS | 1988