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Space Launch System (SLS) Structural Dynamics Analysis

Supporting NASAís Space Launch System (SLS), Dynamic Concepts, Inc. performs loads and structural dynamic assessments of the integrated vehicle and its elements.  DCIís efforts include integrated vehicle loads analysis, flight loads reconstruction, finite element modeling (FEM), hydroelastic fluid modeling, and structural test support.  The integrated loads analysis includes loads simulations for the rollout from the VAB to the pad, prelaunch pad stay, liftoff, boost phase flight, core stage flight, thrust oscillation, and various off-nominal events.  Further details of DCIís support of SLS Loads and Dynamics are provided in the links below.  

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