Preliminary identification and evaluation of promising LO2/Hydrocarbon rocket engine cycles were used to produce a consistent and reliable data base for vehicle optimization and design studies. cycles G and C were chosen for design analysis. Preliminary design analysis of the heat transfer subsystem was performed to establish major technology requirements.


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    Title :

    Advanced oxygen-hydrocarbon rocket engine study


    Contributors:
    Obrien, C. J. (author) / Salkeid, R. (author) / Mueggenburg, H. (author) / Ewen, R. L. (author)

    Publication date :

    1980-08-11


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Advanced oxygen-hydrocarbon rocket engine study

    Obrien, C. J. / Ewen, R. L. | NTRS | 1981


    Advanced Oxygen-Hydrocarbon Rocket Engine Study

    C. J. Obrien / R. L. Ewen | NTIS | 1981



    Advanced Oxygen-Hydrocarbon Rocket Engine Study

    C. J. Obrien / R. Salkeid / H. Mueggenburg et al. | NTIS | 1980