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Update Mass Flow Rates For Aluminum Design #2

@Blueorchid

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@Blueorchid

Hi, at some point we need to update the mass flow rates to match the new aluminum design.

Total propellant flow rate: 2.06 lb/s
Ethanol flow rate: 0.94 lb/s
LOX flow rate: 1.13 lb/s

Not sure if it would be beneficial to combine the injector and the nozzle Jupyter notebooks into one someday, or keep them separate.

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