The report describes the intent and capabilities of the computer program which was developed to evaluate preliminary duty cycles for missile systems, develop specifications for the control system being employed, preform preliminary design analysis on any of the control options, and predict the performance capability of a vehicle utilizing the control system characteristics obtained from the program. The seven potential control inputs are liquid injection thrust vector control, hot gas thrust vector control, gimbal ring, ball and socket, flexible seal, jet tabs, and aerodynamic surfaces. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Advanced Thrust Vector Control Preliminary Design Computer Program. Volume II. User's Manual


    Contributors:
    L. F. Carter (author) / D. P. Dahle (author) / A. R. Randall (author) / C. W. Vogt (author)

    Publication date :

    1972


    Size :

    376 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English