I'm not sure if this is the right forum for this question; feel free to move it if it should go elsewhere...
Back in Orbiter 2010, there was a very lovely and ambitious project called To The Moon in 24 Hours, which proposed nuclear powered rockets that would fly directly toward the moon and directly back, rather than following the slower Hohmann Transfer orbit. The sci-fi series The Expanse uses a similar method of flight to the planets (as their rockets are much more powerful than today's rockets and they can afford to), flying toward their target until they get to a halfway point, then turning and burning the other way to slow down (and using the thrust to produce artificial gravity, as well).
Is there a way, using the MFDs we currently have for Orbiter, of calculating such direct routes?
Back in Orbiter 2010, there was a very lovely and ambitious project called To The Moon in 24 Hours, which proposed nuclear powered rockets that would fly directly toward the moon and directly back, rather than following the slower Hohmann Transfer orbit. The sci-fi series The Expanse uses a similar method of flight to the planets (as their rockets are much more powerful than today's rockets and they can afford to), flying toward their target until they get to a halfway point, then turning and burning the other way to slow down (and using the thrust to produce artificial gravity, as well).
Is there a way, using the MFDs we currently have for Orbiter, of calculating such direct routes?