https://github.com/cuspaceflight/fin_optimizer

Designs minimum mass fins based on vehicle flight profile characteristics.
https://github.com/cuspaceflight/fin_optimizer

Last synced: about 1 year ago
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Designs minimum mass fins based on vehicle flight profile characteristics.

• Host: GitHub
• URL: https://github.com/cuspaceflight/fin_optimizer
• Owner: cuspaceflight
• License: mit
• Created: 2022-10-11T16:49:53.000Z (over 3 years ago)
• Default Branch: master
• Last Pushed: 2022-10-11T22:07:24.000Z (over 3 years ago)
• Last Synced: 2025-02-17T10:49:05.081Z (over 1 year ago)
• Language: Python
• Size: 25.4 KB
• Stars: 0
• Watchers: 5
• Forks: 0
• Open Issues: 0
• Metadata Files:
  • Readme: README.md
  • License: LICENSE

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README

          
# fin_optimizer

Designs minimum mass fins based on vehicle flight profile characteristics.

To use correctly - edit the varaibles in global_vars.py

Then run Optimization_Griffin.py to produce the fins.

Assumes fins to end with the rocket body tube.