Re: [tymkoder] PC attachement conf.
Have you seen the video clip in
this thread?
A few thoughts:
We're not necessarily talking about a very low opening speed or time. This might be a terminal deployment, or it might be a go and throw.
If you watch the video linked, you can see that the canopy is being spun by the orbiting PC, despite the bridle not being "spun up" tight.
The negative effect of an orbiting PC is not a result of the bridle twisting. it's a result of the extraction force shifting directions. Imagine if you could do a PCA, and halfway through, run 20 feet to the left, then run back 20 feet to the right. It's a bit like that. The canopy moves toward the PC (or anchor point, if fixed). When the PC (or anchor point) moves, the canopy changes direction in mid-deployment. This can also lead to slack developing in the system while it moves to line stretch, as it changes directions.
The multi bridle slides--it doesn't necessarily peel. It can slide back up the lines and still remained mostly closed. That means that force can be exerted sideways (kind of like crossloading your risers by dipping a should during deployment) from the instant the PC reaches bridle stretch.