General Specifications:

  • Butanol & Liquid Oxygen
  • Combustion Pressure : 1380 kPa
  • Combustion Temperature: 3000 °C
  • Thrust 2.22 kN
  • Specific Impulse (sea level) : 255 s
  • Burn Time Capability: 20 Seconds
  • Regenerative & Film Cooling Approach

This project is currently active, and being pursued rigorously by four senior project students. The specifications for this engine are suitable for competing in the Spaceport America Cup. 

Hot fire is scheduled for Spring 2018.