Re: Frisbee time
Thanks for mentioning that. If the weight distribution is like a dumbbell, this is said to be "having a high polar moment of rotation", which means that once spinning - frisbee style - it is going to be almost impossible to stop.
This means the craft as shown in the artist's renderings has TWO major problems.
1) Huge asymmetrical thrust in an engine-out event, instant frisbee (yaw) and uncorrectable by any aerodynamic means (i.e instant disaster). While there will need to be attitude thrusters for out-of-atmosphere pitch, roll, and yaw changes, they won't be able to compensate for a main engine failure, and that tiny little vertical stabilizer/rudder is far too inadequate even at lower altitudes.
These are very powerful engines, and if one of them fails, the remaining engine's thrust at the end of a long arm is going to whip the craft around instantly and very vigorously, so yes, we're all going to die. Relax, it will be quick. Very quick.
2) Engines at the rear, as in DC-9 and Lear might result in an aft CG at zero fuel, and I do remember that most aircraft are not "empty tubes" but are full of people and things so the CG doesn't shift drastically - but in this case, if most of the fuselage is fuel tank, the aft CG will be a problem.
Lets put the engines close together, mounted near the CG of the aircraft, probably over (Honda jet) or under (ME-262) the wings. We don't want them so close together that a failure in one will propagate to the other (as in TU-144 and B-70), but we do want them as close as possible to the longitudinal center line of the aircraft so we don't wind up with the asymmetrical thrust problem.
All aircraft are a collection of compromises flying in formation. This particular drawing seems to have been done by a publicist, any aeronautical engineer would reject this configuration in a heartbeat.
I do support this project and hope they are ultimately successful, but I doubt the final aircraft is going to look very much like the picture.