Compatibility measurements were made for aluminum 2219-T87 alloy and titanium 6Al-4V alloy in the presence of liquid fluorine and flox. Results of post test characterization after exposure durations of 61 and 70 weeks are presented. Results of the total test program are analyzed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Compatibility testing of spacecraft materials and space-storable liquid propellants


    Contributors:

    Publication date :

    1974-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :




    Earth-storable propellants for spacecraft

    Dipprey, D.F. | Engineering Index Backfile | 1965



    Development testing of non-toxic, storable hypergolic liquid propellants

    Funk, J. / Heister, S. / Humble, R. et al. | AIAA | 1999