Plasma plume characterization of electric solid propellant pulsed microthrusters

Keyphrases

• Plasma Plume 100%
• Microthruster 100%
• Electric Solid Propellant 100%
• Propulsion 66%
• Cm(III) 33%
• Solid State 33%
• Electron Temperature 33%
• Electric Current 33%
• On Demand 33%
• Velocity Estimate 33%
• Vacuum Level 33%
• Peak Electron Density 33%
• Thruster 33%
• Nude 33%
• Triple Langmuir Probe 33%
• Ionization Fraction 33%
• Residual Gas Analysis 33%
• Re-ignition 33%
• Single Langmuir Probe 33%
• Exhaust Velocity 33%
• Faraday Probe 33%
• Ablated Mass 33%
• Accidental Ignitions 33%
• Ion Current Density 33%

Engineering

• Ignition 100%
• Plasma Plume 100%
• Electron Temperature 50%
• Torr 50%
• Centerline 50%
• Thruster 50%
• Residual Gas 50%
• Exhaust Velocity 50%
• Ion Current Density 50%