Path: Orbit/StraightLine
% Returns data structure for straight line functions
If you enter d it will return a latex formatted version
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Form:
d = StraightLineDataStructure
l = StraightLineDataStructure( d )
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Inputs
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d (.) Data structure
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Outputs
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d (.) Data structure
.dF (1,1) Final distance (km)
.tF (1,1) Final time (s)
.eta (1,1) Thrust efficiency
.sigma (1,1) Specific power (W/kg)
.uE (1,1) Constant exhaust velocity (km/s)
.f (1,1) Tank fraction (kg/kg)
.mD (1,1) Dry mass (kg)
.mF (1,1) Fuel mass (kg)
.m0 (1,1) Initial mass (kg)
.thrust (1,1) Thrust (N)
.accel (1,1) Accel (km/s^2)
.tS (1,1) Thrust sign switch time (s)
.v0 (1,1) Initial velocity (km/s)
.vS (1,1) Switch velocity (km/s)
.dV (1,1) Total delta velocity (km/s)
.p (1,1) Power (W)
.useAccel (1,1) If true is acceleration for simulations
.constPower (1,1) If true hold power constant
or
l {:,3} Latex formatted data structure
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Common: Database/Constant
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