Path: StraightLine/Straight2D
% Dry mass of vehicle from thrust: payload + engine + fuel tanks
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Form:
mass = DryMass( 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) Dry mass, kg
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StraightLine: Straight2D/EnginePower StraightLine: Straight2D/Straight2DStructure
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