Bi-propellant micro-rocket engine

Engineering

• Rocket Engine 100%
• Mass Reduction 33%
• Energy Engineering 33%
• Limitations 33%
• Propulsion System 33%
• Control Systems 33%
• Power Constraint 33%
• Small Satellite 33%
• Orbit Control 33%
• Micro Propulsion 33%
• Feed Pressure 33%
• Micro Turbine 33%
• Cooling Channel 33%
• Maximum Operating Temperature 33%
• Micropump 33%
• Electrical Power 33%
• High Thrust 33%
• Mass Ratio 33%