Hello all,
I am working on a research project which involves sending a spacecraft into the outer solar system. As part of this, I need to investigate the various transfer orbits between Earth and the destination (probably Mars, although this might change). Universe Sandbox seems to be a good tool, although I am after some input in terms of functionality. Can this software account for a small object of given mass (the spacecraft) and, when selecting the destination from Earth, calculate the required transfer orbit?
Appreciate the help.
D.