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I have seen several High powered rockets that use plywood centering rings. I have seen a few Medium power rockets that use plywood centers.
True.
Plywood is stronger, but also heavier. And more expensive.
For what it is, with all the parts, transitions, and wraps, Saturn V kit is a steal at either $90 MSRP, or $54 from ACsupply.com, and a few other places selling it at 40% discount.
At that price point, Estes had to keep costs down, and if cardboard rings are sufficient, they certainly would not be spending more money on plywood!
On the Estes Saturn V here, I was very surprised that the only rated motor is the D12-3. The model is so big, that I understand the need for a quick ejection charge. But I wondered why an E motor was NOT specified.
You may be misinterpreting the purpose of the advertised engine recommendation.
The suggested motor printed on an Estes box is never the largest, but rather, then smallest motor that is safe to fly. If it says D12 (not anymore, minimum recommended for new SatV kit is E12/E30), than means don't even think about launching it on C11!
Nothing is stopping you from going with bigger motors, but those cost more $$, so Estes leaves it up to you as to how much $$ you want to burn (pun intended) with each launch.
My guess is that Estes engineers were concerned about the stress an E motor would put on the frame (as designed). Consequently, I am also concerned about using an E motor, although I intend to use the Aerotech E15W-4.
Nope, nothing to worry about w.r.t. airframe integrity.
Recall that the thrust is transmitted to the airframe from the motor mount, through the centering rings (CRs). There are 3 of those on SatV, so you are transmitting the thrust to the main airframe through 3 circles of 3.9" diameter x 3.14 = 12.25" circumference (for each of 3). Assuming your glue fillets are 1/4" wide (at least) hold, the probability of tearing the 12.25" * 1/4 * 3 = 9.2 inch^2 worth of attachment surface area is just about nil.
You might be concerned with CR deflection under thrust, if so, consider gusseting them, or using stronger materials (additional CRs glued together, book cover, 1/8" plywood, etc).
I had some 1/4" plywood CRs lying around.
They are an overkill, but I used them anyway, mostly because I up-scaled my MMT to 29mm, and happened to have those CRs on hand (see pic below).
I apologize if I'm hijacking the thread here, but I am also building the exact same Saturn V kit. I converted the mount to a 5 engine cluster with a central 29 mm and four 24 mm outboards. I'm confident the thicker 4'' LOC tube can deal with the launch loads, but the cluster requires a considerable amount of nose weight for stability, on the order of 300 grams, which seems like it would be a lot for the upper section to either during launch or under chute. Did I over reach with the cluster, or have others used that much nose weight with success?
One of my MMT configurations will also be a 5-cluster: center 24mm, and 4 outboard 18mm.
The extra tubes (not glued yet) pushed the motor mount (MMT) assembly weight form 33g to 66.3g. Maybe make that +50g of extra mass in the aft part of the rocket when everything is done.
But, my heavy duty 29mm tube with 1/4" plywood CRs weights in at 138g (I over-built this a bit), thus my 5-engine cluster is still lighter than my I-motor ready 29mm MMT.
To keep stability at 1.0 caliber, I need 104g of ballast in the nose cone/command module (vs. 29g stock).
Your MMT may be a bit heavier, but I don't see why you would need 300g of ballast.
HTH,
a