Space Launch System (SLS) Structural Dynamics Analysis
Supporting NASA’s Space Launch System (SLS), Dynamic Concepts,
Inc. performs loads and structural dynamic assessments of the integrated
vehicle and its elements. DCI’s 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 DCI’s support of SLS Loads and Dynamics are provided in the links
below. |
