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But if you intend to scan/ survey you might cover more ground going opposite. I suppose it depends on the mission.
That said though our moon rotates once a monthish so how much difference could it be?
Definitely don't want to enter Jool the wrong way if you are heading for a moon there ha ha.
The only thing I can think of is that you are a bit confused on what it means?
It sounds like you burn out to in front of it and then the mass pulls you to slow you down from its orbital speed and that would put you more retrograde to the Muns motion around Kerbin. This would make for an easier return or possibly a "free" return if you hooked it right with the gravity assist.
This situation is to your advantage if you are doing a flyby and not going into orbit around the Mun.
So it isn't for a retrograde orbit around the Mun but to apply a retrograde vector relative to Muns orbit around Kerbin.
If I am understanding the whole "free return" thing properly.
https://astronomy.com/news/2018/05/why-apollo-flew-in-a-figure-8
My problem is, I'm going around the mun in the retrograde direction. Or as the article above put it (thank you by the way) around in the trailing edge (I think).
So this means that when I do my orbital insertion, I am doing it on the trailing edge of the mun which means that the retrograde vector of my orbit is facing in the direction the mun rotates.
So as I do the orbital insertion, I burn retrograde which means that I'm slowing myself down in the direction of the muns rotation. So the prograde vector is in a direction OPPOSITE the muns rotation, therefore orbit is retrograde (when I look at orbital info it says inclination is around 180 degrees). But would this have been how the apollo missions did it? They would have gone around the trailing edge of the moon and surely must have done their orbital insertion there as this is where their perilune would have been, right? So then the same thing would have happened that would have happened in KSP and their orbit would be retrograde.
Sorry if I'm being confusing, it's just something that's been bugging me a bit recently.
Thank you very much :)
https://forum.kerbalspaceprogram.com/index.php?/topic/48448-effect-of-retrograde-mun-orbit-for-apollo-styled-mission/
I found this conversation on the forums
Always interesting to have something to think about.
So thanks!
the Apollo missions used a free return trajectory because there was concern about the Luna engine reignighting. If it failed the crew could safely return to earth.