Path: Orbit/StraightLine

% Size a spacecraft from acceleration data
 Some combinations of parameters will not converge and the mission will
 be impossible for the given maximum acceleration, which is used to
 compute the maximum thrust and therefore the power plant size. You will
 get an error if it does not converge. 

 Payload mass includes everything that is not engine, fuel or fuel tanks.

 This does not have any outputs, it just draws a plot.

   SpacecraftFromAccel( sC, s )

   sC  (.)
           .uE     (1,1) Exhaust velocity (km/s)
           .sigma  (1,1) Specific power (W/kg)   
           .mP     (1,1) Payload mass (kg) 
           .fS     (1,1) Fuel structural fraction
           .eff    (1,1) Engine thrust efficiency
   s   (.)
           .a      (3,:) Acceleration profile (km/s^2)
           .t      (1,:) Times corresponding to a



Propulsion: Rocket/RocketMass
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Math: Linear/Mag

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