Dozy...
"You may say what you like, although the transition to a rapidly-unwinding altimeter despite the nose-high attitude should have provided a clue"
Knock it off. I am discussing transition through apogee, and the crew have already experienced 1.65 g in the ascent... An acceleration back to 1g from what had been a decreasing ascent, does NOT qualify as airframe STALL WARN, especially,as before, when the nose remains at Extremely high AOA....
Last edited by Lyman; 3rd August 2012 at 22:39.