To post you must either be a member for 30 days and have 20 posts or be a supporting member. 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 Aftershock ii has officially become the highest and fastest amateur rocket of all time
Rocket Reyna : Solofun171
After a thorough internal review, the.
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). Model rocketry enthusiast forum & rocket for sale classifieds Rocketry forums for experts & beginners Engines, recovery, electronics, rocketry software.
This version continues the development of a simplified cfd workflow, with some other features thrown in This workbench can be added to freecad using the addon manager Improved defaults for running cfds directly from rockets (including openrocket and rocksim imports). The rocket will be updated to allow it to use 24mm e motors and have ttw fins
Doug bertelsen and boyce aerospace hobbies have worked on the 3d printing of the camera
I'm hoping that the files will be posted for everyone to enjoy soon Estes cinerocdv and omega (redshifted) (modified 1974 catalog photo markings) Select any part of the rocket and click the cfd button The dialog allows you to set the rocket angle of attack (aoa), and the number of processors you're going to use when running your cfd simulation
This creates a solid version of your rocket and places it in a virtual wind tunnel. I have a tall/thin rocket with a fineness (aka aspect ratio or length to diameter ratio) of ~26 (80” long 3.1” diameter) As currently configured, it has a stability margin of 3.7/14.6% in openrocket Hi everybody , i'm planning to make a two stage sounding rocket that will go to 38km high and i'm analysing options for booster separation
These either requiere the rocket to have a certainly speed to work or a heavy supporting structure to enable the deployments
