SecondRow
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The link doesn’t work for me.Microsoft Word - Document1
This is Tripoli stand on metal in rockets. Please read the entire document if in doubt.
The link doesn’t work for me.Microsoft Word - Document1
This is Tripoli stand on metal in rockets. Please read the entire document if in doubt.
Never rely on the CG calculated by the program. It's fine to get a rough idea, but there are things you can't weigh that can affect the CG, like paint. After my rocket is done and painted, I find the CG by balancing the rocket on the edge of a ruler. Measure that point from the front of the nose cone and put in an override for the CG. Weigh the final configuration (with recovery components, without a motor) and place that in the override as well. The CP will be calculated fair enough by the program, since that is dependent on dimensional data (airframe size, length, nose cone design and fin design and size). You can do a swing test to find the CP, but it really isn't necessary if you use OR or Rocksim and you don't have a wacky design.Yes all the components were measured on weight scale and the input data is 100% correct. The same goes for the dimensions of all components. As for the ground support equipment there is a photo below. (ignore the rocket on the photo because it is from a previous launch after which I made some modifications). For ignition I use cable with kanthal wire inserted into the nozzle of the engine. As power supply I use car battery.
View attachment 514318
In addition to the comments on rod length and the motor's thrust curve, this rocket is pretty short and it has fairly large fins for it's size. How windy was it? This bird is likely to weathercock a lot in winds upwards of 10 mph (17 kph). Adding that to short rod and low thrust and wacky happens.Hello to everyone! I'm fairly new to model rocketry and I recently made couple of homemade rockets from scratch. However when I launched them, every single one of them went crazy immediately after leaving the launch ramp. I used OpenRocket software to design the rockets and the program is telling me that the rocket should be stable. On the last launch (video uploaded as zip) the rocket had a static margin of 1,18cal. On the previous launch I even added some weight to the nose to move the CG and to separate it from the CP. The static margin was 1,83cal. Unfortunately I got the same result as in the last launch. Here's also a screenshot from open rocket design and some photos from the last rocket and I can provide additional information if needed. (NOTE: all the photos bellow are related to the launch shown on the video) Can anyone tell me what may be the possible problem?
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I agree with this just by looking at the deposit in the nozzle. It probably produced asymmetric thrust causing it to become unstable.I watched the video.. it looks to me like the thrust of the motor isn't inline with the rocket c/l... it's shooting out at an angle.
And that would explain the non linear flight pattern.
Maybe try a commercially made motor... fly it as a heads up flight and see what results you get.
This post is fine, but please do not ask or post specifics on your motor. ie…….No formulas.
Clarification: The NAR and TRA rules vary and so do local laws and regulations. High power and model rules are different also. Metal fins and sugar motors are not forbidden. Formulas are forbidden to be discussed on the forum. There is room for discussion what minimal required metal is, but people fly rockets with metal fins at TRA launches where the local club allows them.
This is NOT "fine" with the NAR ( "EX motor" ) . . . And, for HPR, one must be certified, whether NAR, TRA, or CAR.
Dave F.
Yes, you say correctly, it has to do with one another, but on the other hand - who should take care of it?Looks like the launch rod is fiberglass. They tend to have alot of flex. As far as whats allowed or not depends on local rules. If he is not a member of an association like NAR/Tripoli then those specific rules wouldn't apply to him, would they? Not saying he should skirt around safety either way.
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