Path: Propulsion/Electric
% Computes the total mass, fuel mass and power for an electric thruster. -------------------------------------------------------------------------- Form: [mT, mF, p] = FElectricPropulsion( uE, sF, sP, mP, eta, f, dV ) -------------------------------------------------------------------------- ------ Inputs ------ uE (1,:) Exhaust velocity (m/s) sF (1,1) Structural mass ratio (mass structure/mass fuel) sP (1,1) Specific power (mass power/watt) mP (1,1) Payload mass (kg) eta (1,1) Efficiency f (1,1) Thrust (N) dV (1,1) Delta v (m/s) ------- Outputs ------- mT (1,:) Total mass (kg) mF (1,:) Fuel mass (kg) p (1,:) Power (W) --------------------------------------------------------------------------
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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