Nitrogen tetroxide and blend of hydrazine and unsymmetrical dimethyl hydrazine evaluated in rocket engines with large area ratio nozzles - Apollo project


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    Title :

    Experimental rocket performance of Apollo storable propellants in engines with large area ratio nozzles


    Contributors:

    Publication date :

    1966-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English