- #36
Danger
Gold Member
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That sounds basically right to me, with one minor difference. In fact, I'm having trouble understanding why anything that interferes with airflow would be ever be deployed above 0.8 or maybe 0.9 Mach. Transonic shock was why everyone but a few dreamers believed that no object could ever exceed the speed of sound; once past it the ride smooths out. It's less decelerating through than accelerating, but still present. I'd expect such deployment to be roughly equivalent to an Airbus 380 or something similar dropping the gear and flaps and popping the spoilers while still at cruise speed. Survivable, perhaps, but hardly advisable.Astronuc said:I'm a bit puzzled by the comment that the descent system "was deployed prior to Mach 1.4". It would seem the aerodynamic forces would be greater as velocity increases, but I can imagine that the transonic region would experience a fair amount of buffeting.
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