We know that the Spaceship One and Spaceship Two designs from Virgin Galactic/The Spaceship Company/Scaled Composites employ feathering for aerobraking and maneuverability. I can't seem to track down any information on when or exactly how (beyond 'hydraulics') the transitions occur in the flight profile.
At what velocity or altitude does the ship transfer from the 'capsule' configuration to the 'plane' configuration and also what is the orientation of the plane with respect to the nose and atmosphere?
Does it reach the plane configuration in a dive which it must then pull out of or does it transfer to a plane in belly-down freefall where the hydraulic feathering must push against substantial drag?

Also, what's etiquette here? Do I accept your answer or leave it for now since it's basically "we don't know yet" and see if we can find out something conclusive in the next couple of years?
– randomUsername Apr 09 '18 at 21:38