Digging through the article again, it appears that even in normal service (as opposed to delivery from the factory), the passenger version will have 50m less than the freighter; probably because of the lower weight.Ma Deuce wrote:Freighters require shorter takeoff distances than liners, because relieved of the concerns of passenger safety and comfort, they can affort to subject the aircraft to higher pitch/roll conditions.
So they did.If you didn't notice, they did give a graph showing the takeoff distance at various weights...
So I looked it over again.
They did not give any of the values necessary to determine the validity of the graph (all those pretty letters in Figure 5).
But they did admit that they did not know the actual values:
Since Airbus seems to believe that 3300m will be enough at 540t, and this appears to be well below the graph, I'd recommend not to rely on that research paper too much.Since the A380 aerodynamic coefficients are not known, they has been determined for comparison (regression analysis) with other aircrafts. Therefore the validity of the numerical results obtained in this research are subordinated to the real values that the aircraft will achieve in the homologation tests.
As for the added passenger bulk - building larger terminals should be politically much easier than building more runways...