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