The report documents work accomplished under contract F04611-71-C-0013. Ths program discussion 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, perform 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 program has the capability to determine the thrust magnitude required to fly any one of the six types of trajectories where thrust vector and thrust magnitude control is required. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Advanced Thrust Vector Control Preliminary Design Computer Program. Volume I. Program Description. Book 1. Requirements


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

    Publication date :

    1972


    Size :

    652 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English