Path: StraightLine/ConstantThrust
% Fuel mass 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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See also: ComputeThrust
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StraightLine: ConstantAccel/StraightLineDataStructure StraightLine: ConstantThrust/ComputeThrust StraightLine: ConstantThrust/SimulateStraightLineTrajectory Common: Database/Constant
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