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The decision of a particular model of solid rocket motor nozzle control precision and flexible functioning of the pivot center drift and systems for power moment problems, using computer-aided design and analysis methods, and establish flexible nozzle coupled rigid-flexible multi-body dynamic model; to role of the body in the system activity for work on the axial load resistance, for sine wave, rectangular...
The thrust vector control (TVC) system is mechanical power equipment of solid propellant rocket motor. Components of TVC have been produced elasto-plastic contact deformation under loads. The contact problem is belonged to boundary non-linear problem and has no analytical solution. Thus, the method to solve contact problem of TVC joints is 3D modeling by Pro/E, analysis by ANSYS and simulation ground...
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