TTrnsHoh:

Path: Orbit/OrbitMechanics

% Computes the Hohman transfer time between two orbits

   Since version 1.
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   Form:
   T = TTrnsHoh( R1, R2, mu )
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   ------
   Inputs
   ------
   R1                    Orbit radius 1
   R2                    Orbit radius 2
   mu                    Gravitational parameter

   -------
   Outputs
   -------
   T                     Transfer time (sec)

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	References:	Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988,
               pp. 292.
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