So in thinking about the aborted booster landing from CRS 16 a while back (the one with the locked grid fin that went in the spin), I have a question as to how it was corrected.
From Elon's comments, he said the engine worked to overcome the rotation of the booster. The captured video does indeed show the engine gimbaling madly and the booster does slow or even stop rotation just prior to the water touchdown.
My question is how? With a single center mounted engine that can gimbal, how was it able to correct for rotational momentum? It would seem that would require something offset form center, otherwise you'd only be able to correct for yaw or pitch.
If this has already been covered, my apologies... any pointers appreciated.
Thanks.
From Elon's comments, he said the engine worked to overcome the rotation of the booster. The captured video does indeed show the engine gimbaling madly and the booster does slow or even stop rotation just prior to the water touchdown.
My question is how? With a single center mounted engine that can gimbal, how was it able to correct for rotational momentum? It would seem that would require something offset form center, otherwise you'd only be able to correct for yaw or pitch.
If this has already been covered, my apologies... any pointers appreciated.
Thanks.