Path: StraightLine/ConstantThrust
% Compute engine mass given straight-line thrust
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Form:
mass = EngineMass( thrust, d )
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Inputs
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thrust (1,1) Thrust, N
d (.) Data structure
See Straight2DStructure
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Outputs
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mass (1,1) Engine mass, kg
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StraightLine: ConstantThrust/EnginePower StraightLine: ConstantThrust/Straight2DStructure
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