Successful middle run in the testing phase whose purpose was to investigate remote electric ignition of the flame. Good consistent combustion and appreciable thrust considering the low calorific value of the fuel. All work was done by the senior design team of the Vanderbilt University Aerospace Club

Zach Smith, Paul Allen, Christopher Lioi, Thomas Hardy, Tyler Hannan, Taylor Stevenson

Fuel: alcohol
unobstructed diffuser inlet

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