Plume characterization of electric solid propellant pulsed microthrusters

Keyphrases

• Plume 100%
• Microthruster 100%
• Electric Solid Propellant 100%
• Electron Temperature 66%
• Low Temperature 33%
• High Temperature 33%
• Neutral Species 33%
• Thermal Equilibrium 33%
• Propulsion 33%
• Thermoelectric Properties 33%
• Electric Current 33%
• On Demand 33%
• Ion Species 33%
• Vacuum Level 33%
• Thruster 33%
• Chemical Combustion 33%
• Nude 33%
• Plasma Plume 33%
• Triple Langmuir Probe 33%
• Ionization Fraction 33%
• Residual Gas Analysis 33%
• Non-equilibrium Gas 33%
• Re-ignition 33%
• Adiabatic Expansion 33%
• Electric Propulsion 33%
• Flight Data Analysis 33%
• Exhaust Velocity 33%
• Coaxial Pulsed Plasma Thruster 33%
• Faraday Probe 33%
• Ablated Mass 33%

Engineering

• Electron Temperature 100%
• Low-Temperature 50%
• Nonequilibrium 50%
• Thermal Equilibrium 50%
• Centerline 50%
• Electric Propulsion 50%
• Thruster 50%
• Residual Gas 50%
• Plasma Plume 50%
• Pulsed Plasma Thrusters 50%
• Exhaust Velocity 50%

Physics

• Solid Propellant 100%
• Electron Energy 33%
• Photoelectric Emission 33%
• Residual Gas 33%
• Electrostatic Probe 33%
• Electric Propulsion 33%
• Ignition 33%
• Exhaust Velocity 33%