In this paper, the applicability of dual stage ion opticsand in particular of the so-called dual stage ion engine to highpower, high specific impulse missions will be evaluated. First, theperformance limits of conventional two gridded ion engines (GIE)will be discussed and the advantages provided by dual stage ionengines reported. The limits of applicability of a dual stage ionengine will be analyzed analytically and the results confirmednumerically. The lifetime and performance of a three griddeddual stage ion engine (DS3G) will be numerically investigated andcompared to those of a conventional GIE assessing for the firsttime in the open literature under what condition dual stage ionoptics provide performance improvements over conventional...
The transition from OLD SPACE to NEW SPACE along with increasing commercialization has a major impac...
For more than 30 years, NASA has conducted an ion propulsion program which has resulted in several e...
The work performed on the Ion Propulsion System Technology Task in FY90 is described. The objectives...
Ion thruster technology offers the highest performance and efficiency of any mature electric propuls...
The Annular Ion Engine (AIE) concept represents an evolutionary development in gridded ion thruster ...
The NASA Glenn Research Center ion-propulsion program addresses the need for high specific-impulse s...
Some space flight missions require advanced ion thrusters which operate at conditions much different...
Electric propulsion system proven to be a suitable and efficient alternative for conventional propul...
Electric propulsion system proven to be a suitable and efficient alternative for conventional propul...
on thrusters have seen application on space science missions and numerous satellite missions. Ion en...
Advances in high-power photovoltaic technology have enabled the possibility of reasonably sized, hig...
on thrusters have seen application on space science missions and numerous satellite missions. Ion en...
Studies have indicated that xenon ion propulsion systems can enable the use of smaller earth-launch ...
A new and innovative type of gridded ion thruster, the “Dual-Stage 4-Grid ” or DS4G concept, has bee...
Complex space missions involving formation flying or drag compensation are driving the need for spac...
The transition from OLD SPACE to NEW SPACE along with increasing commercialization has a major impac...
For more than 30 years, NASA has conducted an ion propulsion program which has resulted in several e...
The work performed on the Ion Propulsion System Technology Task in FY90 is described. The objectives...
Ion thruster technology offers the highest performance and efficiency of any mature electric propuls...
The Annular Ion Engine (AIE) concept represents an evolutionary development in gridded ion thruster ...
The NASA Glenn Research Center ion-propulsion program addresses the need for high specific-impulse s...
Some space flight missions require advanced ion thrusters which operate at conditions much different...
Electric propulsion system proven to be a suitable and efficient alternative for conventional propul...
Electric propulsion system proven to be a suitable and efficient alternative for conventional propul...
on thrusters have seen application on space science missions and numerous satellite missions. Ion en...
Advances in high-power photovoltaic technology have enabled the possibility of reasonably sized, hig...
on thrusters have seen application on space science missions and numerous satellite missions. Ion en...
Studies have indicated that xenon ion propulsion systems can enable the use of smaller earth-launch ...
A new and innovative type of gridded ion thruster, the “Dual-Stage 4-Grid ” or DS4G concept, has bee...
Complex space missions involving formation flying or drag compensation are driving the need for spac...
The transition from OLD SPACE to NEW SPACE along with increasing commercialization has a major impac...
For more than 30 years, NASA has conducted an ion propulsion program which has resulted in several e...
The work performed on the Ion Propulsion System Technology Task in FY90 is described. The objectives...