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| Setup Tab |
For our example the Setup will look like the screen capture below.
Notice that for our example we already have two inputs set based on our model from Mass Properties.
For the Propellant information the analysis needs either the LoadDensity (propellant density) or Propellant Mass. For our example, since we modeled the propellant the Propellant Mass is known. If the Propellant Mass was not known, then we could enter the propellant density and the ChamberVolume and the program will calculate the Propellant Mass.
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