Small scale liquid rocket engine optimization. Created by Ben Holland and Josh Schechter for the Colorado School of Mines Physics Department senior design.
##Mission Definition: Design and fabricate a liquid oxygen (LOX) and Aviation Kerosene (Jet A) liquid fueled rocket engine with a minimum efficiency of 90% and a thrust of 400 kg. ##Engine Requirements: Engine must be: *Safe to operate for a minimum of 500 firings *90% fuel efficiency *Produce 400 kg of thrust *Interface with mechanical ground support equipment