A small inductively coupled plasma source has been developed for use in an ion thruster. A 10.1-mm-diameter thick film silver spiral antenna is fabricated on a low-temperature cofired ceramic with a 35- $muhbox{m}$ dielectric over the antenna. The antenna has been able to sustain an argon plasma over a frequency range from 448 to 1020 MHz with pressures ranging from 50 mtorr to 1.75 torr. Plasma start powers ranged from 3 to 50 W with minimum sustain powers down to 0.1 W. Antenna electric field measurements have been made in air and compared with simulation of the antenna field using COMSOL. These results show that the antenna pattern is dominated by the standing wave pattern of the spiral antenna. Simulations of the RF power density versus...
Optimization of radiofrequency (RF) plasma sources for the development of space thrusters differs fr...
An Inductively-Coupled Plasma excitation with internal antenna is characterized. The main Plasma is ...
This thesis describes an experimental investigation into the performance of a radio frequency plasma...
A small inductively coupled plasma source has been developed for use in an ion thruster. A 10.1-mm-d...
A miniature electrostatic thruster is being developed in Low Temperature Co-fired Ceramic (LTCC) at ...
An ion thruster for small satellites is under development. The thruster uses an Inductively Coupled ...
[Abstract] A magnetically enhanced inductive discharge was investigated for electric propulsion appl...
Abstract An investigation was conducted for a very small helicon plasma source of a 2.5 cm i.d. glas...
An inductively coupled plasma (ICP) source enabling high-density plasma generation was developed for...
We have developed a cylindrical RF plasma source by the inductive coupling of multiple low-inductanc...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76472/1/AIAA-2008-5199-925.pd
A miniature electrostatic thruster has been developed in Low Temperature Co-Fired Ceramics (LTCC) at...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
In the past twenty years plasma-based propulsion systems have found increasing aerospace interest; a...
Intense ion beam production is of high importance for various versatile applications from accelerato...
Optimization of radiofrequency (RF) plasma sources for the development of space thrusters differs fr...
An Inductively-Coupled Plasma excitation with internal antenna is characterized. The main Plasma is ...
This thesis describes an experimental investigation into the performance of a radio frequency plasma...
A small inductively coupled plasma source has been developed for use in an ion thruster. A 10.1-mm-d...
A miniature electrostatic thruster is being developed in Low Temperature Co-fired Ceramic (LTCC) at ...
An ion thruster for small satellites is under development. The thruster uses an Inductively Coupled ...
[Abstract] A magnetically enhanced inductive discharge was investigated for electric propulsion appl...
Abstract An investigation was conducted for a very small helicon plasma source of a 2.5 cm i.d. glas...
An inductively coupled plasma (ICP) source enabling high-density plasma generation was developed for...
We have developed a cylindrical RF plasma source by the inductive coupling of multiple low-inductanc...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76472/1/AIAA-2008-5199-925.pd
A miniature electrostatic thruster has been developed in Low Temperature Co-Fired Ceramics (LTCC) at...
An ion thruster for satellites on the order of 10-50 kg in mass is currently under development. The ...
In the past twenty years plasma-based propulsion systems have found increasing aerospace interest; a...
Intense ion beam production is of high importance for various versatile applications from accelerato...
Optimization of radiofrequency (RF) plasma sources for the development of space thrusters differs fr...
An Inductively-Coupled Plasma excitation with internal antenna is characterized. The main Plasma is ...
This thesis describes an experimental investigation into the performance of a radio frequency plasma...