Path: Orbit/StraightLine
% Fuel masss for a constant thrust electric propulsion system.
Assumes constant exhaust velocity and constant thrust. Flyby and stopping are
supported. This uses a straight line model.
Type MassFuelElectricConstantThrust for a demo.
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Form:
d = MassFuelElectricConstantThrust( d0 )
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Inputs
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d0 (.) Data structure
See StraightLineDataStructure
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Outputs
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d (.) Data structure with updated fields
See StraightLineDataStructure
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AC: ACData/ACTConstants Orbit: StraightLine/SimulateStraightLineTrajectory Orbit: StraightLine/StraightLineConstantThrust Orbit: StraightLine/StraightLineDataStructure Orbit: StraightLine/StraightLineOptimalFixedUE Orbit: StraightLine/SwitchTime Orbit: StraightLine/UToMF SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/DistanceLabel Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Math: Integration/RK4
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