Rschub
Well-Known Member
Everything is a compromise.
On your run of the mill sport rocket, so what?And the downside is, it's draggy.
TP
Do you want more altitude for a given amount of noise, or more noise for a given altitude? For the latter criterion, mount the rocket on the rail upside down.
You can substitute "money spent" for "noise" in the sentence above. Or you can substitute "speed" for "altitude".
For cert flights when there are limitations on altitude, gratuitous drag makes sense. So they're an exception to what I was writing about.@lr64 / @rocket_troy --
There are different mission objectives for different people and varying launch site conditions.
Check out @Rschub's Level 2 Build Thread: Minnie-Magg drag mods for Level 2?
It ( still ) is an entertaining and educational read and IMO, he came up with an ingenious solution to meet his L2 mission criteria.
-- kjh
p.s. Knowing who posted the X-15 tail fins, I looked hard for a hinged spoiler in that wedge airfoil
I think the part about this thread that confuses me is that "if you're not shaping your fins you're wasting money" is a strange hill to die on when there are so many other things that go into maximizing altitude/cost, if that's your thing, and so many other good reasons to fly rockets than to maximize that metric.Me, and anyone who's trying for performance or economy. At least below Mach 1.5 or maybe 2.
How in the heck is one going to prove speed on an L1 flight besides simulations that might not be "that good" for a particular situation? Some flying sites, it's better to use an H in a heavier rocket for lower apogee, get the L1 cert in otherwise a "screamer rocket" would be lost. Nothing wrong with that.For cert flights when there are limitations on altitude, gratuitous drag makes sense. So they're an exception to what I was writing about.
Personally, if I was dictator, achieving a certain speed or altitude with one's own design and build would be an alternative to using a big motor for certification purposes, as it would demonstrate a certain level of skill and understanding.Say, Mach 1 for level 1.
I think you're right about the electronics and GPS. Miniature dual deploy could help, too. Successful use of these would demonstrate a certain level of mastery, of course.How in the heck is one going to prove speed on an L1 flight besides simulations that might not be "that good" for a particular situation? Some flying sites, it's better to use an H in a heavier rocket for lower apogee, get the L1 cert in otherwise a "screamer rocket" would be lost. Nothing wrong with that.
If one wants to use "screamers" to cert better have electronics, trackers or the rocket will be lost. Especially if it's totally sight unseen. The deployment events might be nominal but if one doesn't see the rocket on descent, won't have a clue where to go to search without a tracker.
I had some totally out of sight flights (not on a cert flight) and for some reason the GPS tracker couldn't get a position out even though I blew the main chute up high (1000ft). I had no idea where the rocket went. I get one ping when the rocket is 75 feet above the ground, walk to that coordinate and there the rocket is!! Still have it though and have flown it many times thereafter and got it back every time.
I always sand my wood fins and for HPR, fiberglassed the smaller rockets with 1/8 oz. fine fiberglass on the fins and sometimes the cardboard bodytubes though it was a PITA as after the fins were glassed, would have to sand them again. Many times I glassed the fins before I epoxied them on the rocket.
I will qualify for larger rockets, I used heavier fiberglass cloth unless they were fiberglass fins and bodytubes to start with.
Have flown small rockets with up to an I-200 and some of my mixed I motors that lord knows what impulse they were. The mixed motors were only at a TRA launches where that was allowed. The NAR launches I only used certed motors and if pre-loaded, brought the motor bag to show the LSO but no one ever questioned me. I never tried anything nefarious either. Kurt
I'm not talking about forcing anything. I'm advocating. Other people are free to go as ugly and/or inefficient as they want. We all claim to be interested in aerospace, where huge amounts of effort are devoted to efficiency.You're talking about forcing people to do things they don't want to do, for no good reason.
I am OCD and want to make everything I build, to borrow a phrase from one of my mentors, "The nicest one of those I can figure out how to make." Between that and my easily-distracted (Ooh, that's a pretty idea!) focus and interest in many things rocketry-related causing me to work on a bunch of different things all at once, my build completion rate is as pathetic as one might imagine, but, man, when I get one done, it's going to be awesome....
Others just want to put something up in the air, and that makes them smile. If square fins make a person smile, fine. Mine will be at least rounded, and usually a lot better than that. Unless I'm using an ARF fin can to make that part of the rocket less OCDified.
I think what's driving this thread is you saying everyone else is wrong for not wanting to do it the way you want to do it. Well, you're wrong about them, right about you. Everyone doing it the way they want to, as long as it is safe, is the right way.
Rather judgmental don't you think?Other people are free to go as ugly and/or inefficient as they want.
One could have a high performance rocket with a removable boat tail. For low performance, substitute an expanding cone.Square edged "airfoils" just look lazy and uncouth, and the edges will quickly wear through the paint. Still, there are some models where you want to increase the drag.
If you're talking about the original Astron Scout that thing has so much fin sweep that it is hard to imagine that the fin profile is that significant, otoh those fins are like 3/16" or 1/4" thick.Actually, it was the high power rockets with square fins that amazed me the most. But there can be significant differences even with the black powder stuff. If we can believe Openrocket, a slightly modified Scout with an Estes C6 will go to 1,808 feet with square fins, 2160 with rounded ones, and 2360 with airfoiled ones.
The foil was one of the modifications. I challenge you to find a swept wing, supersonic airplane that has airfoils anywhere near as thick, in proportion.If you're talking about the original Astron Scout that thing has so much fin sweep that it is hard to imagine that the fin profile is that significant, otoh those fins are like 3/16" or 1/4" thick.
Your continued attempts for intellectual flex, laced with your continued condescension, leaves me scratching me head as to the real point on this thread.The foil was one of the modifications. I challenge you to find a swept wing, supersonic airplane that has airfoils anywhere near as thick, in proportion.
"Flex"???? Not really. It would be silly when I've met a bunch of people smarter than I am. Please put up with what you call my intellectual flex the way I put up with the financial flex of others.Your continued attempts for intellectual flex, laced with your continued condescension, leaves me scratching me head as to the real point on this thread.
I challenge you to offer some actionable intel here, or any tips and techniques that one could employ in the high power/high performance realm. If you are not able to do that, this thread is rather fruitless.
My first rocket was like that. I had some finishing skills from building control line aircraft, but in my youthful rush to fly, I just hand brushed red dope over bare balsa. It was just as well, since it was destroyed by the ejection charge on the first flight.If you really want a low flying rocket- don’t sand the balsa fins, leave them grainy and fuzzy. Then give them one light coat of rattle can spray paint, to get the balsa fuzz to stand up some more and stiffen. Launch it, and watch it ascend to about 1/4 the altitude that you’d imagine it could fly.
A buddy of mine, who does not like to think too deeply about things, and takes the greatest pleasure in “action”, and not “perfection” or results(?) - builds all his rockets this way. I am still amazed at how low he could get his rockets to fly.
True enough, but I've seen some really marvelous workmanship from some really techie people. I've seen some appalling workmanship too, of course.snip
I like the tech stuff, but without the craftsmanship to apply it, it can be pointless.
I've lately started to wonder if the Mach angle is actually relevant to rocket fins, which would typically be too short to intersect the shock cone created by the nose of the rocket, unlike the situation for most supersonic airplanes. Do any of our aerodynamicist members have an informed take on this?Mach angle is arcsin(1/M), where M is the Mach number. For Mach 2, that is 30 degrees, which we generally interpret as a 60-degree sweep back. So you'd want a sweep back > 60 degrees for Mach 2.If I recall correctly, the fins need enough sweep to stay within the shock cone, if that's the right term for it. I think that might mean 63 degrees at Mach 2, though someone with more knowledge should correct me if I'm wrong.
Not ending up with a tiny piece of balsa from trying to sand in airfoils IS hard!Those Reynolds numbers correspond to relatively small rockets. Somehow I missed that you wrote 2 inches, so my comment about big rockets was silly.
Friction drag can be lower if a substantial part of the flow is laminar. My number is based on multiplying the dynamic pressure times the area times the change in drag coefficients.
Sanding balsa into airfoils isn't very hard.
Edit: I calculated again and got 1.8 newtons again. What was the area of your fins?
I've lately started to wonder if the Mach angle is actually relevant to rocket fins, which would typically be too short to intersect the shock cone created by the nose of the rocket, unlike the situation for most supersonic airplanes. Do any of our aerodynamicist members have an informed take on this?
I've lately started to wonder if the Mach angle is actually relevant to rocket fins, which would typically be too short to intersect the shock cone created by the nose of the rocket, unlike the situation for most supersonic airplanes. Do any of our aerodynamicist members have an informed take on this?
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