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. 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. 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 350 lb thrust for five seconds 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). Aftershock ii has officially become the highest and fastest amateur rocket of all time
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. How does open rocket calculate the drag force of the rocket when drag is dependent on cd and cd is dependent on drag force. 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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