As for the lift being too far to the rear, it actually makes for a more balanced design and generally, lower induced drag, since the canard is actually lifting (If it's an All Flying Canard, which it appears to be
It would have to be providing lift. The CoG is way too far in front of the wings for it not to do so.
It just seems that it takes the same issues that the SST suffered from and multiplies them by 3... more weight, most wing lift farther from CoG, longer and pilots even farther from fueslage rotation point.
Maybe the plane will be designed to use the ailerons in conjunction with the canards to make pitch in flight seem less exagerated for the pilots, but no matter how you handle it there, you have to deal with landing a plane with the nose 40 feet off the ground when the rear gear touch.
Its just wierd. I'd really like to see how they have overcome some of the basic issues. I'm sure that aircraft developers that have been doing this for decades have already put most of this in check, but I'm curious as to how they did it.
Possibly.. the fueselage itself is also providing lift? Can't see the bottom profile, but the nose looks more like a leading edge of a wing than the typical "had to end the tube somehow" look of traditional airliners.
AKDejaVu