Add to ORKGExperimental tests results demonstrating that reductions in screen grid thickness enhance the perfor...
Parameter effects on mercury hollow cathode neutralizer performance in ion thruste
Small spacecraft with limited on-board resources would benefit greatly from the development of a low...
The use of dished high perveance grids on a 15 cm modified SERT 2 thruster is shown to facilitate th...
Thrust measurements of a hollow cathode mercury discharge were made with a synthetic mica target on ...
UnrestrictedThis research addresses several concerns of the mechanisms controlling performance and l...
It has been customary to assume that ions flow nearly equally in all directions from the ion product...
The use of electric propulsion systems is growing wider for military and commercial applications, as...
Hollow cathode have recently been investigated at the University of Southampton as potential standal...
The effects of substituting high perveance dished grids for low perveance flat ones on performance v...
Electric propulsion for spacecraft has become increasingly commonplace in recent decades as designer...
Inert gases, particularly argon and xenon, are of interest as possible alternatives to the usual ele...
Abstract: This paper characterizes thrust performance of the T5 hollow cathode and a variant of the ...
Hall thrusters utilize identical hollow cathode technology as ion thrusters, yet must operate at muc...
Performance of four hollow cathode configurations with low work function inserts was evaluated in a ...
Experimental tests results demonstrating that reductions in screen grid thickness enhance the perfor...
Parameter effects on mercury hollow cathode neutralizer performance in ion thruste
Small spacecraft with limited on-board resources would benefit greatly from the development of a low...
The use of dished high perveance grids on a 15 cm modified SERT 2 thruster is shown to facilitate th...
Thrust measurements of a hollow cathode mercury discharge were made with a synthetic mica target on ...
UnrestrictedThis research addresses several concerns of the mechanisms controlling performance and l...
It has been customary to assume that ions flow nearly equally in all directions from the ion product...
The use of electric propulsion systems is growing wider for military and commercial applications, as...
Hollow cathode have recently been investigated at the University of Southampton as potential standal...
The effects of substituting high perveance dished grids for low perveance flat ones on performance v...
Electric propulsion for spacecraft has become increasingly commonplace in recent decades as designer...
Inert gases, particularly argon and xenon, are of interest as possible alternatives to the usual ele...
Abstract: This paper characterizes thrust performance of the T5 hollow cathode and a variant of the ...
Hall thrusters utilize identical hollow cathode technology as ion thrusters, yet must operate at muc...
Performance of four hollow cathode configurations with low work function inserts was evaluated in a ...
Experimental tests results demonstrating that reductions in screen grid thickness enhance the perfor...
Parameter effects on mercury hollow cathode neutralizer performance in ion thruste
Small spacecraft with limited on-board resources would benefit greatly from the development of a low...