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- Where there are dead guys to dig up
With the afterburners on, you will accelerate much quicker and will be able to get off the ground before you run out of ruway easily.
With an empty bay, definitely, lighting the burners is more than sufficient to reach Vr. But with 6-7mt in the bay, the nose won't lift until a much faster groundspeed is achieved, which can't be obtained in the length of the runways at the Cape, burners lit or otherwise.
I think this is just a geometry issue at the moment. (Or a UCD thing. Anyone know how it accounts for mass and its affect on axial rotations? It may be adding the mass in the right place on the G42, but grossly overestimating the forces required to move that mass around using only the '42's control surfaces.) 6mt isn't much mass, but placed where it is so far forward of the center of lift, you can't get enough combined action between the elevators driving the tail down and the canards pushing the nose up until a much higher Vr speed.
At any rate, I admit mine is a flawed experiment, in that I don't know the designed estimates for maximum takeoff mass, or Moach's plans for the future. He could very well be planning for the addition of flaps, or afterburner nozzle vectoring to help drive the tail down, or a way to tie the aileron control in with the elevators to effectively double the surface area of the control surfaces for the take-off run. Personally, I'd love to see two "take-off assist rocket pods" mounted somewhere on the lower portion of the forward fuselage, angled at about 45 or so upwards and fired only when one pulls back on the stick to rotate the nose off the ground (probably not terribly practical ... but damn if it wouldn't look sweet!)
Anyhow, I'm just trying to get a jump on the orbital operations side of things, by experimenting with up-mass potential now rather than later. And the only real deterent thus far is getting the nose to want to come up. Once there is even a minimal positive AoA, she flies and climbs just fine.
