Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Evaluation of 7.8-Inch-Throat-Diameter Inserts and a Unique Cooling Concept in a Storable- Propellant Rocket Engine


    Contributors:

    Publication date :

    1969


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English