Add to ORKGHigh temperature liquid mercury cathodes for ion thrusters - thermal design analysi
Hot-ion hydrogen plasma experiments were conducted in the NASA Lewis HIP-1 magnetic mirror facility ...
Doubly charged ion current measurements in the beam of a SERT II thruster are shown to introduce cor...
Lanthanum Hexaboride (LaB6) hollow cathodes have been found in electric propulsion applications sinc...
Poiseuille flow measurements for high temperature liquid metal cathode ion thruster
Optimization testing of thermally integrated liquid mercury cathode thruster syste
The effects of 8 cm thruster main and neutralizer cathode operating conditions on cathode orifice pl...
Improvements in 15 cm diameter, SERT II, mercury ion thruster performance effected by the use of SHA...
Discharge chamber studies for mercury bombardment ion thrustors - discharge properties effects on ma...
A number of space missions were proposed which utilize 30-cm mercury bombardment ion thrusters and a...
The startup reliability of a 15 cm diameter mercury bombardment ion thruster which employs a pulsed ...
An investigation of the high voltage pulse ignition characteristics of the 8 cm mercury ion thruster...
Experimental tests results demonstrating that reductions in screen grid thickness enhance the perfor...
The measured ion beam divergence characteristics of two and three-grid, multiaperture accelerator sy...
Hollow cathode operation and plasma discharge in mercury ion engine, potential distribution of glow ...
The Mercury Ion Thruster Technology program was an investigation for improving the understanding of ...
Hot-ion hydrogen plasma experiments were conducted in the NASA Lewis HIP-1 magnetic mirror facility ...
Doubly charged ion current measurements in the beam of a SERT II thruster are shown to introduce cor...
Lanthanum Hexaboride (LaB6) hollow cathodes have been found in electric propulsion applications sinc...
Poiseuille flow measurements for high temperature liquid metal cathode ion thruster
Optimization testing of thermally integrated liquid mercury cathode thruster syste
The effects of 8 cm thruster main and neutralizer cathode operating conditions on cathode orifice pl...
Improvements in 15 cm diameter, SERT II, mercury ion thruster performance effected by the use of SHA...
Discharge chamber studies for mercury bombardment ion thrustors - discharge properties effects on ma...
A number of space missions were proposed which utilize 30-cm mercury bombardment ion thrusters and a...
The startup reliability of a 15 cm diameter mercury bombardment ion thruster which employs a pulsed ...
An investigation of the high voltage pulse ignition characteristics of the 8 cm mercury ion thruster...
Experimental tests results demonstrating that reductions in screen grid thickness enhance the perfor...
The measured ion beam divergence characteristics of two and three-grid, multiaperture accelerator sy...
Hollow cathode operation and plasma discharge in mercury ion engine, potential distribution of glow ...
The Mercury Ion Thruster Technology program was an investigation for improving the understanding of ...
Hot-ion hydrogen plasma experiments were conducted in the NASA Lewis HIP-1 magnetic mirror facility ...
Doubly charged ion current measurements in the beam of a SERT II thruster are shown to introduce cor...
Lanthanum Hexaboride (LaB6) hollow cathodes have been found in electric propulsion applications sinc...