Modified electro-thermal thrust augmentation for mini-satellite applications

Keyphrases

• Ceramics Heater 33%
• Compact Design 16%
• Cost Reduction 16%
• Electrical Energy 16%
• Electrical Resistance 16%
• Gaseous Products 16%
• Heater 33%
• Hydrazine 16%
• Hydrazine Decomposition 16%
• Limited Power 16%
• Microsatellites 16%
• Minisatellite 100%
• Monopropellant 16%
• Performance Improvement 16%
• Performance Penalty 16%
• Pulse Train 16%
• Resistance Heater 16%
• Silicon Carbide Ceramics 16%
• Specific Impulse 33%
• Thermal Losses 16%
• Thermoelectric Properties 100%
• Thrust Augmentation 100%
• Thrust Level 16%
• Thruster 100%
• Thruster Design 16%
• Variable Duty Cycle 16%
• Weight Reducing 16%

Engineering

• Duty Cycle 14%
• Electrical Power 14%
• Internals 14%
• Performance Penalty 14%
• Pulse Train 14%
• Simplifies 14%
• Specific Impulse 28%
• Thruster 100%