I have the kit and have modeled in open rocket using exact measurements and having weighed each part With a stock build, and adding 50 grams of clay nose weight, i'm getting a ground hit velocity. I hope this post finds you all soaring high in your rocketry adventures I'm a high school student currently navigating through the fascinating world of water rocketry for my research paper My focus is on the optimization of water rocket fins in terms of their size. Aftershock ii has officially become the highest and fastest amateur rocket of all time
After a thorough internal review, the. The advanced rocket will be multi stage rocket projects but has a new set of flight challenges Flight computers and or altimeters to help with dual.deploy, cable cutters, recording the flight parameters, tracking devices to help find the project. Long story short i just got my level 1 over the weekend and flew it low and slow But now i might like to reach for the stars as it were lol I'm terrified of losing my rocket though and am contemplating investing in some sort of tracking system
Hello everyone, i would like to introduce you to a gyroscopic stabilization system which i made.the system is designed to prevent the rocket from rolling These are for one time sales items, no business sales To post you must either be a member for 30 days and have 20 posts or be a supporting member. We’re a university team just getting started with building model rockets, and one of our main goals is to develop an active control system We’re currently debating between using movable fins (canards) or thrust vector control (tvc). For example, this will not be the desired result if the rocket comes out of the pad and after it spins around a bit and stabilizes the angle at which it rotates
How can i determine the correct choice of canards for a rocket going 2 mach It is really difficult to guess how the canards selected with the created program control the rocket. These either requiere the rocket to have a certainly speed to work or a heavy supporting structure to enable the deployments If the objective is to minimize weight and for the deployment to occur as far and as close at apogee as possible, wouldn't this rocket extraction method be very practical I would love to know your opinion
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