LowThrustDVToTransfer:
% Compute delta-v assuming full thrust applied during all transfer times.
--------------------------------------------------------------------------
Form:
[dVTot,dVElem] = LowThrustDVToTransfer( dT, m0, thrust, Isp )
--------------------------------------------------------------------------
------
Inputs
------
dT (5,1) Transfer times for each orbital element (sec)
See LowThrustTimeToTransfer.m
m0 (1,1) Initial mass of spacecraft (kg)
thrust (1,1) Thrust magnitude (kN)
Isp (1,1) Specific impulse (sec)
-------
Outputs
-------
dVTot (1,1) Total delta-v for changing all elements (km/s)
dVElem (5,1) Delta-v for changing each element (km/s)
--------------------------------------------------------------------------
