Fore Check
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- Sep 24, 2010
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Ok, so I'm cooking up something here, and I've run into a design quandry of sorts.
My motors will be a 4 x 24mm cluster in a BT80. This section of BT80 will be a net 8.5" long.
The airframe above this motor can will be BT70, about 30" long. The will be coupled using centering rings, not a transition. The BT70 can stick up to 4" inside the BT80, which would put the bottom end of the BT70 about 3/4" in front of the tops of the cluster mount (it will be 3.75" long for E engines.) This means that the airframe reduction will occur very close to the tops of the motors, and there will be no stuffer tubes running up through the BT70 (you can't fit 4 x 24mm in a BT70 anyway.)
I could possibly reduce the amount of BT70 that is inside the BT80 to 3" giving a bit more "relief" above the cluster mount before it is reduced a bit (again via centering rings), but would prefer not to just from an overall rigidity standpoint.
Does anyone see any problem with this? Am I asking for trouble, or should it work no problem?
Here's another idea I'm kicking around that ties in with this.
In order to keep the laundry forward in the airframe close to the NC, I was thinking about taking a 1/4" thick plywood centering ring to fit inside the BT70 that has a center hole *at least* large enough for a BT60 to pass through it. I'd glue this in the BT70 about 12 - 13" in from the forward end of the airframe. I'd lay a couple of small dowels (1/8" or so) in an "X" pattern across the opening in the aforementioned centering ring. I figure this would provide a "bottom" of sorts for wadding and laundry to stop at and stay above during a launch, but also let the ejection gasses pass through. Note that regular Estes type wadding would be used, in large loosely crumpled balls, as opposed to dog barf.
I'm opposed to using a piston arrangement because there's already a reduction in airframe above the engines, and I feel that a piston would further complicate things.
Again, any input on these ideas would be appreciated.
My motors will be a 4 x 24mm cluster in a BT80. This section of BT80 will be a net 8.5" long.
The airframe above this motor can will be BT70, about 30" long. The will be coupled using centering rings, not a transition. The BT70 can stick up to 4" inside the BT80, which would put the bottom end of the BT70 about 3/4" in front of the tops of the cluster mount (it will be 3.75" long for E engines.) This means that the airframe reduction will occur very close to the tops of the motors, and there will be no stuffer tubes running up through the BT70 (you can't fit 4 x 24mm in a BT70 anyway.)
I could possibly reduce the amount of BT70 that is inside the BT80 to 3" giving a bit more "relief" above the cluster mount before it is reduced a bit (again via centering rings), but would prefer not to just from an overall rigidity standpoint.
Does anyone see any problem with this? Am I asking for trouble, or should it work no problem?
Here's another idea I'm kicking around that ties in with this.
In order to keep the laundry forward in the airframe close to the NC, I was thinking about taking a 1/4" thick plywood centering ring to fit inside the BT70 that has a center hole *at least* large enough for a BT60 to pass through it. I'd glue this in the BT70 about 12 - 13" in from the forward end of the airframe. I'd lay a couple of small dowels (1/8" or so) in an "X" pattern across the opening in the aforementioned centering ring. I figure this would provide a "bottom" of sorts for wadding and laundry to stop at and stay above during a launch, but also let the ejection gasses pass through. Note that regular Estes type wadding would be used, in large loosely crumpled balls, as opposed to dog barf.
I'm opposed to using a piston arrangement because there's already a reduction in airframe above the engines, and I feel that a piston would further complicate things.
Again, any input on these ideas would be appreciated.