1 / 5

School Name

Team Name. School Name. Rocket design diagram with measurements. Include drawing of rocket identifying all components Include measurements of air frame and fins. Identify the number of fins. Total weight of rocket with payload Location of CP Location of CG Materials list.

genera
Download Presentation

School Name

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Team Name School Name

  2. Rocket design diagram with measurements • Include drawing of rocket identifying all components • Include measurements of air frame and fins. • Identify the number of fins. • Total weight of rocket with payload • Location of CP • Location of CG • Materials list

  3. Recovery Harness • Show drawing of recovery harnesses for each part of rocket • Identify harness material and strength • Identify linkages and load limits • Identify eye bolts and mounting methods

  4. Altimeters • Show wiring diagram of altimeters • Document altimeter preparation steps • Specify the quantity of black powder to be used and the volume to be pressurized and calculated pressure level • Specify how sections are secured before ejection charges separate sections • friction fit • shear pins • other • Identify how charges are set off • e-matches • flash bulbs • other

  5. Motor Selection • Identify primary motor selection • Calculate thrust to weight ratio • thrust ratio must be a minimum of 5:1 • Identify back up motor selection • Calculate thrust to weight ratio • thrust ratio must be a minimum of 5:1 • Attach simulation plots for each motor and expect weight

More Related