Is birch ply generally used as fin material in HPR? I too have found it to be... well, not extremely robust, although I do like it for LPR centering rings. Similar issues to what @Off Grid Gecko reports, although it is pretty stiff.
Is birch ply generally used as fin material in HPR? I too have found it to be... well, not extremely robust, although I do like it for LPR centering rings. Similar issues to what @Off Grid Gecko reports, although it is pretty stiff.
Is birch ply generally used as fin material in HPR? I too have found it to be... well, not extremely robust, although I do like it for LPR centering rings. Similar issues to what @Off Grid Gecko reports, although it is pretty stiff.
Totally agree and I give this a lot of thought. I'm familiar with fin flutter, just don't know all the mathematical details. Hopefully the 1/4" fins are stiff enough to prevent most of it and strong enough to tolerate any that might develop in future flights as I push the rocket faster than I will on it's initial launches.Just for technical thought practice, Consider also the difference between your test setup and a real flight.
A motor applies an impulse or short sharp amount of thrust (force) to a free moving rocket that responds by accelerating (hopefully upwards). Additionally the tubes, coupler joints, and fins are subject to dynamic stresses due to the airflow. For further learning, research fin flutter.
Your test is applying a Static load over a sustained time, and the rocket is prevented from accelerating, so it has to absorb all that force and stress within its structure (probably for longer than itll see any of it in flight)
Epoxy-coated 3 of the fins last night, prolly will do the other one this evening.
I don't know how much a 1G Cesaroni case weighs, or if it is worth the bother.
Thanks again for the input. Yes, structurally I'm sure the 1/4 ply has it in that department, but the wood is quite brittle, so the epoxy is really to keep small chunks from splitting out on a hard landing rather than adding any kind of extra structural integrity. Just a skin to keep everything together.How thick are your fins? I hate to say it late in the game, but they were likely plenty strong without the added epoxy weight.
The relatively low-aspect clipped delta design you've used is very stable at high speeds.
As you fly more, you'll begin to learn the limits and strengths of the materials you use, and your builds will get leaner (better overbuilding in the beginning than underbuilding). One thing I find annoying as an engineer is the lack of material data for the common things we use in rocketry which makes it difficult to do meaningful analysis without making a handful of -ish assumptions, and not having a personal wind tunnel to validate.
On flutter, the tool FinSim is a good resource to use if you're willing to do some reading about the proper inputs and interpreting the outputs.
Unless I'm mistaken, you won't be finding drag coefficients info from the barrowman equations. Their purpose is to aid in locating the CP, not determining component drag coefficients. (and unless I'm mistaken, flutter and divergence are more driven by Lift on the fins than drag)
Regardless, your rocket is looking great and will no doubt surprise you in how much motor it can take. If you're using OpenRocket, the motor selection page should list the full loaded weight (as well as empty weight) and that includes casing.
Blank page and first draft are great names. Maybe L2 can be "Revision" and L3 "Final Cut"
Always a possibility. All glued up, I'm looking at 1233g with the thicker mid-section. Primer, filler, paint? And four screws to secure the mid section to the fin can, tiny ones but another couple grams. A 29mm LMS might be the way to go for small flights. I haven't used an adapter before, but I'm sure I could make it work with the retaining cap. The other issue is 80N of thrust pushing the rocket, for a TWR of just over 5:1, it should be fine on a 6-8 foot launch rail...I think. I'll need to run the numbers.The G78 blue is just a hair under 200 grams. If you're on the edge on weight, you might look at a 29mm Aerotech single use (technically LMS) at 125 grams plus another 25-50 grams for a 38mm-29mm adapter. If you have lots of stability, shaving a little off the length is a good way to go to minimize weight.
I figured that many of these motors spikes quite quickly and then dropped off the thrust. I may look closer at the G motors and the range from 1G to max thrust. I assume it would be fairly linear, so no need to do an integral. I should be able to plot it out on a spreadsheet easily enough. I definitely don't mind the math that goes with rocketry, but I hadn't thought that it would take half a second for a motor to ramp up. I'll keep that in mind when it comes time to shop.Light coat of filler primer, sand most of it off, light coat of paint?
You can get a general estimate of rail exot speed* using a spreadsheet, its just tedious to import the thrust curve of the motor you want to analyze each time. That is important since the motors often thrust above or below their average thrust number during the time the rocket is on the rail. Thats where thrustcurve.org can help with its batch run of all motors that fit. (Make sure you tell it the mmt is longer than the motor or it wont run that motor). Thrustcurve will flag your flight as "red" if rail exit speed is below 50ft/s, but with no to low wind, and a rocket that isn't understable, you can go down to ~45ft/s
Example: using the AT G78, it ramps up to 80N thrust over 1/2 second (medium propellant, Mojave Green I think) compared to the AT G80 that puts out 100N almost instantly (Blue Thunder, fast propellant).
*Account for effective rail length being the tip of rail to forward rail button. Once that front button is free, the rocket can yaw.
Hehe, naw, I at least need to do some kind of paint job. I can make krylon do wonderful things sometimes, when I get lucky and I don't have a nozzle that blasts big blobs.Thats almost as tall as my biggest motor case! Lol
I rather like the various sanded coatings, wood grain, and exposed tubing look. A couple coats of clear coar will preserve it, and not weigh too much either.
Why screws? Does that section need to be accessible?
I have the names "Motivation" and "Inspiration" reserved for a future 2-stage high-altitude rocket, which go back to one of the books I wrote, and motivation just makes a nice name for a booster Thinking about doing one of those pieces as an L2 or L3 project and then attaching the second part for a trip to Black Rock.
I used 25000. found some numbers online ranging from 20k-30k and split the difference just to get a rough idea. There could be a weak point in there, but in general I would hold that something a 1/4 inch thick is going to have a pretty uniform stiffness. I think they are making a bigger deal of that point than it needs to be in the article. Like all the calculations to determine Mach speed which amount to very little change from day to day. I suppose if you are trying to be really precise and fly at the bare minimum requirements, then that would become more important, but for ballpark figures it hardly seems necessary. Just plug in 1100 and go, lol. I can't ever picture myself trying to tune down my fins to within 50 ft/s of the flutter calculation, when there are much bigger problems to worry about in rocket design. They should always be strong.Hmmm, what did you use for G (shear modulus) of 3 ply plywood? It doesnt exactly meet the isotropic properties condition of the apogee article
The book I referred to was called "Finish the Damn Book!" and written as a motivation source for writers. It's by far my best selling title (i.e. making enough money to buy me a taco each month, lol). If you look that one up on Google then you'll be led to my other titles on Amazon. Here are some of the titles:I like those names, hope you build that one day. I'm curious, what books did you write?
I realized what it was while looking at the mfg website last night. They only have KwikWeld at the local store. I ran to town this morning for some other stuff and picked up paint and original JBWeld which has the 550F resistance. Might put on the retainer tonight and let it cure while I sleep.Can you take a pic of the JB you bought?
The reason JB steel-weld (original) is used on retainers is because they're metal. Better bonding properties
Here's the base coat laid down. This paint works a bit better than the normal primer, so it's actually hiding quite a bit I think. Most of the tube is in alright shape, but the nose is a little weird. Good enough to fly I think, and it looks good from about 20 feet away.
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