| Summary: | The research concerns the computational analyses of local strength of the umbilical mast (UM), which is designed for the prelaunch preparation and launch security of the space rocket (SR) "SOYUZ-2" of 1B stage.Based on the finite elements method, modeling and calculation of local strength for the most loaded UM elements are conducted using Russian program complex «APM WINMACHINE». The paper gives a justification for choosing the program complex «APM WINMACHINE, as a program calculation device.In calculating the principles of a local analysis are used. Physical models of the UM particular constructive units are formed to observe them under certain boundary conditions: forces and movements. Parameters of boundary conditions are determined in terms of stress-strain condition of UM simplified model as a whole.As the research results, the paper presents the finite element models of two UM constructive units, namely a joint of the mast farm branches with strengthening of the mast rotating part and an element in the UM bottom rotating part (“the spine”). Besides, there are also the calculated results of the local strength of abovementioned UM rotating part units: a general pattern of the stress distribution with stress values exceeding the allowable ones.The research results allow us to draw conclusions that the units under consideration have performance capability and require their constructive strengthening.The UM developers have taken in consideration recommendations, based on the UM rotating part local strength calculation, making appropriate correction in the project documentation. The experience gained in using the «APM WINMACHINE» allowed us to support the conclusion that it is efficient to solve the tasks of defining stress-strain condition of complicated spatial constructions.
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