Monash

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

VIT

Takeaways for RIT Launch Initiative

Do more simulation and analysis. Use ANSYS. Beg ANSYS distributor if RIT doesn't have a license.
Do more physical structural testing.
Insert decision matrix into report.
Do more documentation - all team reports were substantially more detailed.

To Do

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