Originally Posted by
ShyTorque
If the cabin rotates at 130 rpm, this will result in a net loss of 130 rotor rpm. This would almost certainly result in the same outcome - it is a loss of almost half the rotor rpm needed to sustain lift and the integrity of the disc would probably be lost, especially as the aircraft would be descending at a high rate.
Out of interest where does the 130rpm come from?
The only other time I've seen data from an event like this it was about 120 deg/sec.