Path: SpacecraftEstimation/DemoFuns
% Pressure given fuel mass for a blowdown propulsion system.
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Form:
y = GXUKF( x, d )
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Inputs
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mFuel (1,1) Mass of fuel (kg)
d (1,1) Data structure
.mPress (1,1) Mass of pressurant (kg)
.rhoFuel (1,1) Fuel density (kg/m^3)
.vTank (1,1) Volume of fuel (m^3)
.rPress (1,1) Gas constant for the pressurant (m^2/sec^2)/deg-K
.T (1,1) Fuel tank temperature (deg-K)
SC: Actuator/BDDesign SC: Actuator/BloDown SC: Environs/MolWt2R Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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