The test bed fabricated to demonstrate hydrogen/oxygen propulsion technology readiness for the IOC Space Station application is described and test results are presented. The reliability and safety of the O2/H2 system was demonstrated with blowdowns and thruster firings. The flexibility of the system was demonstrated through the addition of an electrolysis supply module.


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    Title :

    Space Station propulsion system test bed and control system testing results


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

    Publication date :

    1987-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    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. | Tema Archive | 1987




    Space Station propulsion system test bed

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