Lampshade111
ACCESS: Confidential
- Joined
- 5 October 2008
- Messages
- 151
- Reaction score
- 17
Are they any good overviews of how the thrust on the X-32B was directed for VTOL purposes? I understand it had two lifting nozzles near the center of the aircraft, and have seen this in many videos. However I always figured there was a third lift nozzle at the rear, just before the main 2D engine nozzle. Can't seem to find it however, were there only two lift nozzles and the smaller pitch/yaw ducts?
I have read that one significant advantage Boeing had was the manufacturing process they would have used to produce their JSF. Did we get anything out of that to implement into the the current Lockheed F-35 program?
I have read that one significant advantage Boeing had was the manufacturing process they would have used to produce their JSF. Did we get anything out of that to implement into the the current Lockheed F-35 program?