Path: StraightLine/ConstantThrust
% Initial mass of vehicle from straight-line thrust and time The initial mass is composed of the payload, engine, fuel, and fuel tank. This depends on the mission duration and engine parameters. -------------------------------------------------------------------------- Form: mass = InitialMass( thrust, d ) -------------------------------------------------------------------------- ------ Inputs ------ thrust (1,1) Thrust (N) d (.) Engine data structure ------- Outputs ------- mass (1,1) Initial mass (kg) --------------------------------------------------------------------------
StraightLine: ConstantThrust/EngineMass StraightLine: ConstantThrust/Straight2DStructure
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