Abstract: We have significantly upgraded the capability of the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) experiment (VX-50) to process over 50 kW of total Radio Frequency (RF) power. The VASIMR system is comprised of three main stages, plasma production using a helicon, ion cyclotron resonant frequency (ICRF) acceleration, and exhaust into a magnetic nozzle. Power capability of up to 30 kW is demonstrated in the plasma source and over 30 kW is coupled into the ICRF stage. Efficient plasma production is achieved with ion-electron pair investment costs of 100 eV. We measure plasma flux exceeding 1021 ion/s. Significant ion acceleration is observed using deuterium, neon and argon. Ion energies in excess of 300 eV are measured, w...
Interplanetary travel requires propulsion systems that can provide high specific impulse (Isp), whil...
The development of a Magnetically Vectored Variable I(sub sp) Plasma Rocket at the Advanced Space Pr...
textThis dissertation was motivated by the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) p...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
In the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) radio frequency (rf) waves both produ...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR™) is a high power magnetoplasma rocket, c...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
The first flight test of the variable specific impulse magnetoplasma rocket (VASIMR) is tentatively ...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
(VASIMR) is a high power, radio frequency-driven magnetoplasma rocket, capable of Isp/thrust modulat...
An efficient plasma source producing a high-density (approx.10(exp 19/cu m) light gas (e.g. H, D, or...
A Variable Specific Impulse Magnetohydrodynamic Rocket (VASMIR) uses two stages of radio frequency e...
A Variable Specific Impulse Magnetoplasma Rocket (VASIMR) uses Ion Cyclotron Resonant Heating (IRCH)...
During this research period the following models of the VASIMR helicon discharge have been further d...
Optimization of radiofrequency (RF) plasma sources for the development of space thrusters differs fr...
Interplanetary travel requires propulsion systems that can provide high specific impulse (Isp), whil...
The development of a Magnetically Vectored Variable I(sub sp) Plasma Rocket at the Advanced Space Pr...
textThis dissertation was motivated by the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) p...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
In the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) radio frequency (rf) waves both produ...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR™) is a high power magnetoplasma rocket, c...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
The first flight test of the variable specific impulse magnetoplasma rocket (VASIMR) is tentatively ...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
(VASIMR) is a high power, radio frequency-driven magnetoplasma rocket, capable of Isp/thrust modulat...
An efficient plasma source producing a high-density (approx.10(exp 19/cu m) light gas (e.g. H, D, or...
A Variable Specific Impulse Magnetohydrodynamic Rocket (VASMIR) uses two stages of radio frequency e...
A Variable Specific Impulse Magnetoplasma Rocket (VASIMR) uses Ion Cyclotron Resonant Heating (IRCH)...
During this research period the following models of the VASIMR helicon discharge have been further d...
Optimization of radiofrequency (RF) plasma sources for the development of space thrusters differs fr...
Interplanetary travel requires propulsion systems that can provide high specific impulse (Isp), whil...
The development of a Magnetically Vectored Variable I(sub sp) Plasma Rocket at the Advanced Space Pr...
textThis dissertation was motivated by the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) p...