Path: Orbit/OrbitMechanics
% Computes the Hohman transfer time between two orbits
Since version 1.
--------------------------------------------------------------------------
Form:
T = TTrnsHoh( R1, R2, mu )
--------------------------------------------------------------------------
------
Inputs
------
R1 Orbit radius 1
R2 Orbit radius 2
mu Gravitational parameter
-------
Outputs
-------
T Transfer time (sec)
--------------------------------------------------------------------------
References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988,
pp. 292.
--------------------------------------------------------------------------
Back to the Orbit Module page