Phase I of the program for a High Performance Oxygen/Hydrogen Rocket Engine is an evaluation of the critical technology associated with the staged-combustion bell-nozzle engine system. Experimental evaluation is being conducted in the areas of the main burner, turbopump bearings, engine controls, and the preburner. In addition, engine system (module) preliminary design and application studies are being conducted.


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    Title :

    Advanced Cryogenic Rocket Engine Program Staged-Combustion Concept


    Contributors:

    Publication date :

    1967


    Size :

    190 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English