- 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. We’ve Manufactured the majority of the components, and are close to testing. We are currently waiting on insurance to pursue testing. The specifications for this engine are suitable for competing in the Spaceport America Cup.