Add to ORKGThis paper presents the status of FEEP technology and its application potential for commercial and scientific missions. The thruster development plan, aimed at flight readiness in 1999, is outlined and discussed. Recent results of support development activities, computational simulations and electronics design are presented
Developed at Alta for extremely high performance scientific missions, such as LISA Pathfinder, Field...
Tbe experimental characterization of tbe response of FEEP to variations in time of the applied volta...
This paper presents the results of functional tests carried out on the first 7 em slit FEEP emitter ...
The FEEP thruster development is carried out by Centrospazio under ESA and ASI funding. This activit...
The FEEP thruster development is carried out by Centrospazio under ESA and ASI funding. This activit...
The scientific community’s recent interest in Field Emission Electric Propulsion (FEEP) for drag-fre...
Two interesting fields of applications are envisaged for a miniaturized, modular FEEP thruster: firs...
The scientific community's recent interest in Field Emission Electric Propulsion for drag-free space...
Field Emission Electric Propulsion (FEEP) is presently regarded as the ideal solution for drag comp...
The limited mass and volume available make the development of advanced miniaturized propulsion syste...
Primarily intended for verification of the thruster design and assessment of actual performance, the...
CubeSat development has seen a rise since the first launch in 2003 due to faster design process and ...
Low thrust electric propulsion systems find a promising application field on small-to-medium sized s...
The FEEP thruster is presently considered for several scientific missions requiring micrnnewton-leve...
Field Emission Electric Propulsion (FEEP) thruster has been chosen for a number of future space miss...
Developed at Alta for extremely high performance scientific missions, such as LISA Pathfinder, Field...
Tbe experimental characterization of tbe response of FEEP to variations in time of the applied volta...
This paper presents the results of functional tests carried out on the first 7 em slit FEEP emitter ...
The FEEP thruster development is carried out by Centrospazio under ESA and ASI funding. This activit...
The FEEP thruster development is carried out by Centrospazio under ESA and ASI funding. This activit...
The scientific community’s recent interest in Field Emission Electric Propulsion (FEEP) for drag-fre...
Two interesting fields of applications are envisaged for a miniaturized, modular FEEP thruster: firs...
The scientific community's recent interest in Field Emission Electric Propulsion for drag-free space...
Field Emission Electric Propulsion (FEEP) is presently regarded as the ideal solution for drag comp...
The limited mass and volume available make the development of advanced miniaturized propulsion syste...
Primarily intended for verification of the thruster design and assessment of actual performance, the...
CubeSat development has seen a rise since the first launch in 2003 due to faster design process and ...
Low thrust electric propulsion systems find a promising application field on small-to-medium sized s...
The FEEP thruster is presently considered for several scientific missions requiring micrnnewton-leve...
Field Emission Electric Propulsion (FEEP) thruster has been chosen for a number of future space miss...
Developed at Alta for extremely high performance scientific missions, such as LISA Pathfinder, Field...
Tbe experimental characterization of tbe response of FEEP to variations in time of the applied volta...
This paper presents the results of functional tests carried out on the first 7 em slit FEEP emitter ...