Path: StraightLine/ConstantThrust
% Fuel mass from the thrust and duration -------------------------------------------------------------------------- Form: mass = FuelMass( thrust, d ) -------------------------------------------------------------------------- ------ Inputs ------ thrust (1,1) Thrust (N) d (.) Engine data ------- Outputs ------- mass (1,1) Fuel mass --------------------------------------------------------------------------
StraightLine: ConstantThrust/Straight2DStructure
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