Pressure:
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Computes the REA and tank pressure
Since version 1.
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Form:
[p,pSystem] = Pressure(mFuel,database,temp)
[p,pSystem] = Pressure(mFuel,database)
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Inputs
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mFuel (1,n) Propellant mass per system
database (1,:) Spacecraft properties database
temp (1,n) System temperature
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Outputs
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p (1,m) Thruster pressure
pSystem (1,n) System pressure
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Children:
Common: Database/Constant
SC: Actuator/BloDown
SC: Environs/MolWt2R
