Path: StraightLine/Flyby
% Report of engine properties for a straight-line flyby mission
Compute the payload fraction from the time, distance, and engine
properties. Compute the power requirement from the payload mass. If there
are no outputs the report is printed to the command line.
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Form:
[s,dOut] = FlybyReport( mP, d, doPlot )
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Inputs
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mP (1) Payload mass (kg)
d (.) Structure, see Straight2DStructure
doPlot (1) Flag to print a report despite outputs
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Outputs
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s {:} Latex
dOut (.) Updated data
.p Engine power (W)
.m0 Initial mass (kg)
.mE Engine mass (kg)
.mF Fuel mass (kg)
.mD Dry mass (kg)
.mDot Mass flow rate (kg/s)
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See also: SolveLambdaFlyby
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StraightLine: Flyby/SolveLambdaFlyby StraightLine: Flyby/ZeroPayloadFlyby StraightLine: Straight2D/DryMass StraightLine: Straight2D/EngineMass StraightLine: Straight2D/EngineThrust StraightLine: Straight2D/FuelMass StraightLine: Straight2D/Straight2DStructure Common: General/DisplayLatexTable Common: Graphics/DistanceLabel
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