VEscape:

Path: Orbit/OrbitMechanics

% Computes the escape velocity.

   Type VEscape for a demo of earth escape.

   Since version 1.
--------------------------------------------------------------------------
   Form:
   v = VEscape( r, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   r     (1,:) Radius
   mu	(1,1) Gravitational parameter (default = 3.98600436e5 km^3/sec^2)

   -------
   Outputs
   -------
   v 	(1,:) Escape velocity for a hyperbola

--------------------------------------------------------------------------
   References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988,
               pp. 48.
--------------------------------------------------------------------------

Children:

Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle

Back to the Orbit Module page