Power efficiency estimation of an inductive plasma generator using propellant mixtures of oxygen, carbon-dioxide and argon

Earth and Planetary Sciences

• Propellant 40%
• Power Efficiency 40%
• Argon 30%
• Oxygen 30%
• Carbon Dioxide 20%
• Propulsion 20%
• In Situ Resource Utilization 20%
• Utilization 20%
• Mixture 20%
• Science and Technology 10%
• Frequency Shift 10%
• Ignition 10%
• Compatibility 10%
• Thermodynamic Efficiency 10%
• Monitoring 10%
• Aspect 10%

Physics

• Plasma Generator 100%
• Propellant 40%
• Oxygen 30%
• Carbon Dioxide 20%
• Propulsion 20%
• Mixtures 20%
• Utilization 20%
• Ignition 10%
• Frequency Shift 10%
• Thermodynamic Efficiency 10%
• Technology 10%

Engineering

• Antenna 60%
• Input Power 20%
• Current Measurement 20%
• Inductive Coupling 20%
• Mixture 20%
• Applications 20%
• System Output 10%
• Power Supply 10%
• Experimental Result 10%
• Duty Cycle 10%
• Frequency Shift 10%
• Compatibility 10%
• Thermal Efficiency 10%
• System Input 10%
• Thruster 10%
• Design 10%
• Characteristics 10%
• Estimation 10%