A preliminary design of an advanced LOX/ LH2 expander cycle rocket engine producing 7,500 lbf thrust for Orbital Transfer vehicle missions was completed. Engine system, component and turbomachinery analysis at both on design and off design conditions were completed. The preliminary design analysis results showed engine requirements and performance goals were met. Computer models are described and model outputs are presented. Engine system assembly layouts, component layouts and valve and control system analysis are presented. Major design technologies were identified and remaining issues and concerns were listed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Orbit Transfer Rocket Engine Technology - 7.5K-LB Thrust Rocket Engine Preliminary Design


    Contributors:
    T. J. Harmon (author) / E. Roschak (author)

    Publication date :

    1993


    Size :

    240 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English