Path: Propulsion/Gas
% Generates a blowdown curve of mass vs. pressure. -------------------------------------------------------------------------- Form: [mFuel, density] = GasMass( vTank, mWt, T, p ) -------------------------------------------------------------------------- ------ Inputs ------ vTank (1,1) Tank volume mWt (1,1) Molecular weight of the fuel (default is xenon) T (1,1) Temperature (deg-K) p (1,:) Pressure ------- Outputs ------- mFuel (1,:) Mass of the fuel density (1,:) Density of the fuel --------------------------------------------------------------------------
Common: Graphics/Plot2D SC: Environs/MolWt2R
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