Primarily intended for verification of the thruster design and assessment of actual performance, the FEEP thruster flight demonstration (EMITS - Electrical MIcrothruster Test in Space) is aimed at building confidence in this new technology among the potential commercial and scientific users. EMITS will exploit an existing ESA-NASA agreement for the utilization of the Get Away Special (GAS) facility to fly a package including two thrusters of different thrust levels (30 μN and 1 mN), the thruster power and control electronics unit, a computerized experiment control and data storage unit, and a battery. The main goal of the experiment is the verification of in-orbit ion beam production, neutralization and throttling. Other goals include ion b...
Field Emission Electric Propulsion (FEEP) thruster has been chosen for a number of future space miss...
The Ionic Liquid Field Emission Electric Propulsion (IL-FEEP) thruster is proposed in this thesis wo...
Two interesting fields of applications are envisaged for a miniaturized, modular FEEP thruster: firs...
Primarily intended for verification of the thruster design and assessment of actual performance, the...
The scientific community's recent interest in Field Emission Electric Propulsion for drag-free space...
This paper presents the results of functional tests carried out on the first 7 em slit FEEP emitter ...
The scientific community’s recent interest in Field Emission Electric Propulsion (FEEP) for drag-fre...
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...
Neutralization of the ion beam produced by a FEEP thruster is in principle a task similar to the wel...
This paper presents the experimental setup of the Endurance Test of a Field Emission Electric Propul...
The limited mass and volume available make the development of advanced miniaturized propulsion syste...
This paper presents the design of a novel system for ion beam scanning. The system is equipped with ...
This paper presents the results of a series of tests performed on a set of field emission electric p...
Since the beginning of FEEP research, it was generally believed that the operational field of this t...
Field Emission Electric Propulsion (FEEP) thruster has been chosen for a number of future space miss...
The Ionic Liquid Field Emission Electric Propulsion (IL-FEEP) thruster is proposed in this thesis wo...
Two interesting fields of applications are envisaged for a miniaturized, modular FEEP thruster: firs...
Primarily intended for verification of the thruster design and assessment of actual performance, the...
The scientific community's recent interest in Field Emission Electric Propulsion for drag-free space...
This paper presents the results of functional tests carried out on the first 7 em slit FEEP emitter ...
The scientific community’s recent interest in Field Emission Electric Propulsion (FEEP) for drag-fre...
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...
Neutralization of the ion beam produced by a FEEP thruster is in principle a task similar to the wel...
This paper presents the experimental setup of the Endurance Test of a Field Emission Electric Propul...
The limited mass and volume available make the development of advanced miniaturized propulsion syste...
This paper presents the design of a novel system for ion beam scanning. The system is equipped with ...
This paper presents the results of a series of tests performed on a set of field emission electric p...
Since the beginning of FEEP research, it was generally believed that the operational field of this t...
Field Emission Electric Propulsion (FEEP) thruster has been chosen for a number of future space miss...
The Ionic Liquid Field Emission Electric Propulsion (IL-FEEP) thruster is proposed in this thesis wo...
Two interesting fields of applications are envisaged for a miniaturized, modular FEEP thruster: firs...