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Seeking Insights on Water Rocket Fins Optimization Hello Rocketry Enthusiasts! 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
University team looking for advice: Movable fins or thrust vector . . . Question Hi everyone! 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)
Yard Sale Wanted | Rocketry Forum - Model Rocketry Forums If you have a personal rocketry-related item for sale, or that you're looking for, this is where you list it 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
GPS Trackers for Rocket - Rocketry Forum 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 I know these "egg timers" are suggested but yes
Electronic Gyro Rocket Roll Stabilization System - Rocketry Forum 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 The idea is to use it with rockets that have a built-in camera or other equipment that does not withstand the rolling of the rocket during
Hybrid Rocket Build Thread - Rocketry Forum Hello everyone, I am currently in the process of building a HPR hybrid rocket motor and am posting to get opinions, advice, and help The motor has a theoretical average thrust of 800N 2 Propellant is paraffin wax with carbon black additive 3 Oxidizer is N2O I have already
New Method for Parachute Deployment? Deployment by Rocket Extraction . . . 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 Thank you!