Heat transfer coefficients in rocket nozzle cooling passages predicted by equation developed from hydrogen flow experiments


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A method of predicting heat transfer coefficients in the cooling passages of NERVA and Phoebus-2 rocket nozzles.


    Contributors:

    Conference:

    PROPULSION JOINT SPECIALIST CONFERENCE ; 1968 ; CLEVELAND, OH


    Publication date :

    1968-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English