It seems to me that the Enterprise is still a very inefficient planform (Can I really say "planform" for a spacecraft with no wings that will permanently operate in vacuum?) for a interplanetary long-duration spacecraft.
Even with the low-g constant thrust from ion engines, it seems to me that off-axis masses require at least
some additional structural strength, which means more weight, which means more mass, which means less fuel, less reactor, less crew, less equipment, less shielding for Solar CME's and places like the Jovian radiation belts. And on and on and on.
With a ship that size, the extra trusswork or girders or whatever needed to hold those masses out from each other at oddball angles and away from the main thrust axis of the craft... I'm guessing it adds up. At least it would over a most efficient solution that kept all the major components in line with the main axis of thrust. The one thing I think he gets right though is putting the gravity-wheel habitat for the crew parallel to the main thrust axis. Much like how a current-day Ferris Wheel stands upright against the Earth's gravity. The constant thrust will be light, fractional g, and this will cause the crew to experience a 3x a minute fractional gravity change, but if the crew can adapt w/o sickness or disorientation it might be worth the material/mass savings than mounting it perpendicular to the thrust axis. Although if mounted perpendicular, they could just slant the floor of the wheel habitat areas so the outward centrifugal vector and the average constant thrust vector of the ion engines combines to provide an apparent level surface to the occupants.
Someone would have to do the math on both approaches and decide which is better.
My biggest beef so far... unless I couldn't find it before his site got overwhelmed...
He seems to have totally forgotten radiator panels. Hell, the ISS has radiators that are roughly 1700sqft (maybe more by now with additional modules?), to service the waste heat the energy utilization of the 27k sqft of solar panel, and incidental solar heating generates... (I'm guessing the ISS is always "power thirsty", and waste heat is that big an issue already.) The big reactor pile of this "Mk1 Enterprise" is going to have
huge amounts of waste heat. Even with tech 20 to 100 years in the future it'll never be 100% thermally efficient. The best I've heard fourth-gen reactors (that nobody gets to build due to politics, save for test units, although the Chinese will I guess...) can do is about 45% thermal efficiency, and that's ground based, where there's no mass-fraction to think about. You can build stuff as heavy, or as thick, or as much piping or machinery as you want. Even if it's 75% thermally efficient, (probably a gross overestimation) the 1.5GW fission reactor is going to create 375,000,000 Watts of waste heat.
I suppose some exotic liquid metal cooling system will be possible. But even if it uses liquid sodium, lead.. whatever is the most efficient, I dunno... The radiator "fins" will be BIG.
If the guy is really
that smart, and can plan all of this, I think he
knows about these issues, but wants to keep it looking like "the Enterprise" as long as possible, should he be able to create some sort of groundswell of support from Trek fans, and have the project reach some sort of critical mass before major design changes, or "real" design work gets underway, assuming it ever gets that far.
If true, that implies a certain level of Machiavellian deviousness, which frankly will probably be required should this get anywhere beyond some excited buzz and some web pages.