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)
Advanced Thrust Vector Control Preliminary Design Computer Program. Volume II. User's Manual
1972
376 pages
Report
Keine Angabe
Englisch
Computer Software , Guided missile trajectories , Thrust vector control systems , Programming(Computers) , Design , Rocket motors(Solid propellant) , Advanced planning , Secondary injection , Thrust augmentor nozzles , Nozzle throats , Nozzle inserts , Rocket cases , Mathematical models , Computer programs , Instruction manuals , Computer aided analysis , Computerized simulation