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I hope this post finds you all soaring high in your rocketry adventures 3) how heavy will the rocket weigh approximately ? 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. 2) what material is the shock cord made of 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).

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. 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. 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 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 Hi, i'm curious is there a recommended ratio of rocket length to diameter for the most efficient design? The openrocket team is pleased to release the first public beta for openrocket 24.12 Standard caveats for beta releases apply

We have no known outstanding bugs, but once it gets wider usage issues may crop up, which will be fixed for the final release In the meantime, please give it a spin. 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

Oxidizer is n2o i have already. 1) how large is the rocket

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