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- Telemetry in nosecone
- Airbrakes
- Many points for analysis. Used in-house programmed rigid body simulator SATURN.
- Initial design in OpenRocket. SATURN has substantially lower error, as tested by known data from previous flights. OpenRocket considers slender-finned vehicles using the Barrowman Equations
Berkeley
- Small scale structural testing on CF and glass tubes
VIT
- Fin flutter analyzed using MATLAB
- CF fins cut with waterjet
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