The goal of a 6 dof calculation is to determine the mount stiffness' in the 3 coordinate directions. Conventional software programs take in mount stiffness' as inputs and perform a point calculation. This has to be manually repeated until proper modal decoupling and frequency placement is obtained.
Raptor completely changes this paradigm and uses an objective function called the Modal Optimization Matrix to retrieve the optimal mount stiffness' as outputs. This reduces the time for obtaining a satisfactory mounting system from days or weeks to seconds.
Raptor has a shock calculator that helps design mounts for 1 dof shock applications. The user can calculate velocity shock, elastic and inelastic free falls, and several wave forms.
Raptor uses a unique built-in toolkit for calculating the Mooney Rivlin coefficients for hyperelastic FEA when only the Durometer (Shore A) hardness of the compound is known.
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