Architecture of the integrated systemfor mechanical analysis of spacecraft on-board electronic equipment

The architecture of the expandable integrated system for engineering analysis isdiscussed. The main principles of design for such system are emphasized. The functionality of theintegrated system is divided onto three classes: preparing the initial data, performing calculationsbased on certain methods, and analyzing the results. The module architecture which comprises theadvantages of both the facilities of external CAD/САЕ-systems and own methodical and theoreticalimplementations, is presented. The model of cross-module interoperability based on unifiedprogram interfaces is described. The minimal required set of program interfaces and modules forbuilding the integrated system for mechanical analysis of the spacecraft on-board electronicequipment is mentioned.

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