Simulation Analysis of the Fast Reversing Characteristics of a Certain Carrier Rocket Launcher
By simulating and analyzing the quality characteristics and hydraulic system selection of the actual launch pad,the influencing factors in the rapid reversing process of the rocket launch pad are identified.Combining the drift and roll characteristics of the rocket during takeoff,starting from structural design,equipment layout,cylinder hinge point layout,and reversing tension control,and combining the influence of the reversing and deceleration stage on the stability of the cylinder pressure rod,an implementation plan for realizing the rapid reversing of the launch pad after zero-second ignition of the rocket is proposed,and the analysis results are applied to the design of the actual object.Through practical application verification,the interference of rocket takeoff drift is effectively avoided,the reliability of the launch is improved.
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维普
