I would love if anyone of you could explain why NASA's test of the orion was on an identical inclination of the apollo trajectories and why it required greater shielding for future lunar missions if the apollo shielding was so effective in transiting the VAB and lunar operations. Why fix that which is not broken? How does that work in your mind. Apollo ventured out in solar maximum and received a piddling of an exposure. What was not to love about that?
You are trolling. Many people here have attempted to explain why the trajectories of Orion and Apollo were different and this is the last time I will attempt.
Orion has been built with at least two generations of electronics advanced as those of Apollo. The trajectory of Orion was to test the whether shielding would protect the electronics in the worst environment the engineers could think of the dense proton radiation (if that is the correct term) while Apollo engineers wished to avoid as much of the VARB as they could. It is simple to understand once you get over your ignorance of orbital mechanics. I suggested getting a copy of Kerbal Space Program and one other member suggested it also. Further I suggest you discontinue posting until you have had a little experience with it. You are wrong on so many levels concerning Apollo.
In your next post you requested members join you on Facebook to chat without Abaddon's thoughts, well he may come across a little rough, but he is right on in his ideas. Perhaps he is weary of dealing with likes of HB's. I get a chuckle out of his comments that needle you.