Path: StraightLine/SLPowerLimited
% Compute the transit time and exhaust velocity for constant thrust Pass empty for muF to compute the optimal value which minimizes transfer time. -------------------------------------------------------------------------- Form: [tF,aMax,muE,muF] = TOFLinearAccel(lambda,dF,sigma,muF,f) -------------------------------------------------------------------------- ------ Inputs ------ lambda (1,:) Payload ratio (0-1) dF (1,1) Distance traveled (km), optional sigma (1,1) Jet specific power, W/kg muF (1,:) Fuel mass fraction (mFuel/m0) f (1,1) Fuel tank fraction, optional [0] ------- Outputs ------- tMin (1,:) Minimum transfer time aMax (1,:) Maximum acceleration (m/s^2) muF (1,:) Fuel mass fraction (mFuel/m0) muE (1,:) Engine mass fraction (mEngine/m0) --------------------------------------------------------------------------
Common: Database/Constant Common: Graphics/TimeLabel
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