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About This Project
Nozzle flow separation is a condition where exhaust gases in a rocket nozzle cause severe pressure fluctuations that can damage a spacecraft. The Schmucker Criterion provides insight as to where this flow separation occurs, but it tends to become inaccurate at smaller scales. Using a small scale composite combustion chamber, we want to use vibration data and nozzle extensions to determine exactly what nozzle expansion ratio causes damage to our carbon fiber material during test.
More Lab Notes From This Project
![Blast off!](https://d1sg0ksu7mr16v.cloudfront.net/admin_uploads/emails/April/EFF_rocket.gif)
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