Path: Orbit/StraightLine

% Print a summary of an SLPL problem
 tau is the time in the second half of the trajectory, between the turnaround
 and tF. It is zero for a flyby, tF/2 for a rendezvous, and a value inbetween
 gives a non-zero final velocity.
   [s,dOut] = SLPLReport( Pj, m0, tF, A, tau )
   [s,dOut] = SLPLReport( Pj, m0, tF, A, tau, sigma, f, doPlot )

   Pj       (1,1)    Jet power (eta*P, eta*sigma*mE) (W)
   m0       (1,1)    Initial (wet) mass (kg)
   tF       (1,1)    Final time (s)
   A        (1,1)    Acceleration scale parameter, (m/s^3)
   tau      (1,1)    Time between turnaround and tF (s)
   sigma    (1,1)    Specific power (W/kg)
   f        (1,1)    Tank mass fraction, mTank = f*mF
   doPlot   (1,1)    Always display output

   s         {}      Latex report
   dOut     (.)      Output data structure



AC: ACData/ACTConstants
Orbit: StraightLine/SLPLDeltaV
Orbit: StraightLine/SLPLTrajectory
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeleteCell
Common: General/DisplayLatexTable
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/DistanceLabel
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl

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