The effects of long-term (up to 10 years) contact of inert materials with earth-storable propellants were studied for the purpose of designing chemical propulsion system components that can be used for current as well as future planetary spacecraft. The primary experimental work, and results to date are reported. Investigations include the following propellants: hydrazine, hydrazine-hydrazine nitrate blends, monomethyl-hydrazine, and nitrogen tetroxide. Materials include: aluminum alloys, corrosion-resistant steels, and titanium alloys. More than 700 test specimen capsules were placed in long-term storage testing at 43 C in the special material compatibility facility. Material ratings relative to the 10-year requirement have been assigned.


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    Titel :

    Propellant material compatibility program and results


    Beteiligte:
    Toth, L. R. (Autor:in) / Cannon, W. A. (Autor:in) / Coulbert, C. D. (Autor:in) / Long, H. R. (Autor:in)

    Erscheinungsdatum :

    15.08.1976


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Long-Term Propellant/Material Compatibility

    Clifford M. Moran | NTRS | 1990


    LONG-TERM PROPELLANT/MATERIAL COMPATIBILITY

    Moran, C. M. / United States | British Library Conference Proceedings | 1990