Path: StraightLine/ConstantThrust
% Data structure for straight line mission analysis
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Form:
d = Straight2DStructure
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Outputs
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g (.) Data structure
.tF (1,1) Final time (s)
.dF (1,1) Final distance (km)
.f (1,1) Fuel structural fraction (kg/kg)
.uE (1,1) Exhaust velocity (km/s)
.sigma (1,1) Engine specific power (W/kg)
.eta (1,1) Efficiency, power to thrust
.mP (1,1) Payload mass (kg)
.mE (1,1) Engine mass (kg)
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Common: Database/Constant
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