FlyerTalk Forums - View Single Post - A380 tests the effects of minimum velocity take off (video):
Old Jul 24, 2008 | 2:41 pm
  #9  
Justme123456
 
Join Date: Jun 2005
Location: LAX
Programs: AA, UA, NW, DL, Marriott
Posts: 354
Originally Posted by goalie
way cool tho is it me or is that a pretty long time once the nose comes up to be riding in the mains? (yeah, i know, big plane )
I thought the same thing. Here is a poster's seemingly detailed answer as to some of the dynamics of the test. In addition, there are a couple of other interesting videos on the same page that these comments were made. I will post the link below:
"They put have a special tailskid installed, rotate very early, and gently set the tailskid on the runway. You'll notice the rotation is somewhat quick, yet you don't see sparks until several seconds after the initial rotation has stopped. I imagine there is a tailstrike protection control law which prevented a tailstrike on the initial rotation, then after the initial rotation the protection was shut off, and the tailskid contacts the runway. Then they drag the tail until it lifts off.

Vr speeds are set by several parameters from several different tests, not just an increment from Vmu. You can strike the tail at airspeeds well below Vr if you mistrim the stab and/or yank the stick full aft.

Some test pilots might call Vmu a fun test. In a tail geometry limited plane like this you must accel above stall speed to be able to liftoff, so there's still an increment of margin before stall. Certainly you notice the pilot push to a slightly lower AOA after noticing the increase in AOA after liftoff. If you are all engine, probably no dip in airspeed even with that brief higher AOA part after liftoff..."
http://flyboytv.com/index.php?m=video&v=78
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