Visualization of pulse firing mode in hypergolic bipropellant thruster

Earth and Planetary Sciences

• Pulse 100%
• Firing 83%
• Manifold 50%
• Research 33%
• Time 33%
• Ignition 33%
• Fill 33%
• Investigation 16%
• Surface Pressure 16%
• Mixture 16%
• Injection 16%
• Combustion 16%
• Fuel 16%
• Visualization 16%
• Evaporation 16%
• Oxidizer 16%
• Attitude Control 16%
• Nitrogen Monoxide 16%
• Monomethylhydrazines 16%
• Propellant 16%
• Nitrogen Tetroxide 16%

Engineering

• Thruster 83%
• Research 33%
• Chamber Pressure 33%
• Response Time 33%
• Mitsubishi Heavy Industry 33%
• Measurer 16%
• Evaporation 16%
• Japan 16%
• Demonstrates 16%
• Mixture 16%
• Fuel 16%
• Transients 16%
• Visualization 16%
• Sensing System 16%
• Oxidizer 16%
• Team Member 16%
• Spacecraft 16%

Physics

• Ignition 33%
• Pressure 16%
• Evaporation 16%
• Sites 16%
• Mixtures 16%
• Injection 16%
• Combustion 16%
• Fuel 16%
• Transients 16%
• Attitude Control 16%
• Propellant 16%