Data were computed assuming equilibrium composition during isentropic expansion using normal hydrogen as propellant for chamber pressures from 0.146960 to 1469.60 psia, pressure ratios from 1 to 3000, and chamber temperatures from 600 to 5000 K; performance parameters are given.


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    Title :

    Compilation of thermodynamic properties, transport properties, and theoretical rocket performance of gaseous hydrogen


    Additional title:

    NASA -- Tech Note


    Contributors:
    King, C.R. (author)


    Publication date :

    1960


    Size :

    71 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English