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Juno

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Designed, built, and tested a modular, liquid bipropellant rocket engine capable of 300 pounds of thrust.

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# of Test Fires: 2

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Draco

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Designed, built, and tested a liquid bipropellant feed system rated for cryogenic liquid oxygen.

Juno and Draco Hot Fires

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Hotfire #1: Achieved 300 lbs of thrust

Hotfire #2: Achieved 350 lbs of thrust

Hotfire #3: Ignition occured, but experimental torch igniter failed and caused the test to abort (I designed the platform the torch was mounted to that pivots the torch away from the engine after ignition)

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