Path: StraightLine/ConstantThrust
% Data structure for straight line mission analysis -------------------------------------------------------------------------- Form: d = Straight2DStructure -------------------------------------------------------------------------- ------- Outputs ------- g (.) Data structure .tF (1,1) Final time (s) .dF (1,1) Final distance (km) .f (1,1) Fuel structural fraction (kg/kg) .uE (1,1) Exhaust velocity (km/s) .sigma (1,1) Engine specific power (W/kg) .eta (1,1) Efficiency, power to thrust .mP (1,1) Payload mass (kg) .mE (1,1) Engine mass (kg) --------------------------------------------------------------------------
Common: Database/Constant
Back to the StraightLine Module page