Path: Orbit/StraightLine

% Fuel mass for a constant accel/power electric propulsion system
 Assumes constant power and constant acceleration. The spacecraft slows to zero
 velocity at its target. This uses a straight line model. This model assumes
 power is constant. This means exhaust velocity increases as the mass drops.
 There are two cases in the demo, one for a flyby mission and one for a
   d = MassFuelElectricConstantPower(d0)

   d0    	(.)   Data structure
                 See StraightLineDataStructure
                   .mis  ''  Mission type, 'flyby' or 'stop'
                   .p    (1) Power (W)

   d     	(.)   Data structure with updated fields
                   .a      (1) Acceleration (km/s2)
                   .mF     (1) Fuel mass (kg)
                   .thrust (1) Thrust (N)
                   .uE     (1) Exhaust velocity (N)

  See also MassFuelElectricConstantUE


AC: ACData/ACTConstants
Orbit: StraightLine/StraightLineConstantAccel
Orbit: StraightLine/StraightLineDataStructure
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/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Math: Integration/RK4

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