Research of thermal strains on the reflector with the planimetric directional diagram

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The combined numerical simulation of thermal deformation of the planimetric directional diagram of space vehicle using AnsysWorkbench was implemented. Heat flux data was transferred manually from Thermica software. The comparative analysis of simulation results with prototype data was considered. Technological and economic calculations relatively prototype parameters were made.

Ansysworkbench, antenna space vehicle, reflector, coal-plastic, thermal deformation, technological and economic calculations

Короткий адрес: https://sciup.org/148204998

IDR: 148204998

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