1 / 8

Harvard-Westlake Rocketry Club

Harvard-Westlake Rocketry Club. SLI 2008-2009 FRR. Rocket Stability. Thrust-to-Weight Motor Selection. Thrust: 664.83 N Weight: 82.52 N Ratio: 8.06 8.056 is well above the safe limit of 5. Rail Exit Velocity. According to Rocksim, the Rail Exit Velocity is 42.5174 ft/s

nita-coffey
Download Presentation

Harvard-Westlake Rocketry Club

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. Harvard-WestlakeRocketry Club • SLI 2008-2009 • FRR

  2. Rocket Stability

  3. Thrust-to-Weight Motor Selection • Thrust: 664.83 N • Weight: 82.52 N • Ratio: 8.06 • 8.056 is well above the safe limit of 5.

  4. Rail Exit Velocity • According to Rocksim, the Rail Exit Velocity is 42.5174 ft/s • 42.5 ft/s is above the recommended 30-35 feet per second exit speed.

  5. Parachute Size • Drogue: 24” • Descent Rate: ~60 feet per second, depending • on the final payload mass • Main: 60” • Descent Rate: ~25 feet per second, depending • on the final payload mass

  6. Test Plans • Scale Model Testing • Complete! • Scientific Payload Testing

  7. Test Flight

  8. Avionics and Payload • Avionics testing will be performed with Christmas Tree Lightbulbs at school • The payload will be stored in the electronics bay, simplifying set-up procedures

More Related