Development and testing of ablative rocket engine with selected 7.62 cm /3.0 in./ diameter throat inserts, and testing of zirconia reinforced with tungsten-rhenium wire for throat insert material


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    Title :

    Development and testing of ablative rocket engine with selected 7.62-centimeter /3.0 in/ diameter throat inserts


    Contributors:

    Publication date :

    1971-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English