Advanced Design Problems in Aerospace Engineering, Volume 1: Advanced Aerospace Systems

The gravitational constants for the Sun, Earth, and Mars are given by
Earth and Mars travel around the Sun along orbits with average radii
The associated average translational velocities and angular velocities (inertial coordinates) are given by
In particular, the angular velocity difference between Earth and Mars is
For the outgoing trip, the spacecraft is to be transferred from a low Earth orbit to a low Mars orbit; for the return trip, the spacecraft is to be transferred from a low Mars orbit to a low Earth orbit. The radii of the terminal orbits are
corresponding to the altitudes
since the Earth and Mars surface radii are given by
The circular velocities at LEO and LMO (relative-to-planet coordinates) are given by
and the corresponding escape velocities (relative-to-planet coordinates) are given by