Based on the results of Rocket Motor Sizing utility and a desired peak pressure, the required throat diameter and grain length have been computed and could be manually entered as Rocket Motor Simulation inputs. In our example we instead went back to the model editor and pulled the values from the actual projectile model's geometry. In addition, some desired input parameters are automatically passed through to the Rocket Motor Simulation code.
These values will be noted as we go over the input tabs in this tutorial.
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