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

8: Planetary and Mission Data

8 Planetary and Mission Data

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


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