Add to ORKGThis paper presents work on the application of virtual metrology techniques to the VAriable Specific Impulse Magnetoplasma Rocket (VASMIR) engine. The work concentrates on the estimation of internal temperatures of the rocket using state space models and Optical Emission Spectroscopy (OES). These estimations are useful as direct thermal measurements will not be available in the final system design
Abstract: We have significantly upgraded the capability of the Variable Specific Impulse Magnetoplas...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
Plasma processes can present dicult control challenges due to time-varying dynamics and a lack of r...
This paper presents work on the application of virtual metrology techniques to the VAriable Specific...
The VASIMR propulsion system is an ion propulsion system for spacecraft that uses magnetic fields to...
Interplanetary travel requires propulsion systems that can provide high specific impulse (Isp), whil...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR™) is a high power magnetoplasma rocket, c...
NASAâ s VAriable Specific Impulse Magnetoplasma Rocket Engine (VASIMR) will provide a highly effici...
(VASIMR) is a high power, radio frequency-driven magnetoplasma rocket, capable of Isp/thrust modulat...
To gather information about both particle and gas phase temperatures inside a scaled solid rocket mo...
The article is devoted to the use of plasma rocket engines in open space and their advantages over c...
During this research period the following models of the VASIMR helicon discharge have been further d...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
The following paper outlines the importance of vacuum ultraviolet (VUV) aerothermodynamic heating du...
Abstract: We have significantly upgraded the capability of the Variable Specific Impulse Magnetoplas...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
Plasma processes can present dicult control challenges due to time-varying dynamics and a lack of r...
This paper presents work on the application of virtual metrology techniques to the VAriable Specific...
The VASIMR propulsion system is an ion propulsion system for spacecraft that uses magnetic fields to...
Interplanetary travel requires propulsion systems that can provide high specific impulse (Isp), whil...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR™) is a high power magnetoplasma rocket, c...
NASAâ s VAriable Specific Impulse Magnetoplasma Rocket Engine (VASIMR) will provide a highly effici...
(VASIMR) is a high power, radio frequency-driven magnetoplasma rocket, capable of Isp/thrust modulat...
To gather information about both particle and gas phase temperatures inside a scaled solid rocket mo...
The article is devoted to the use of plasma rocket engines in open space and their advantages over c...
During this research period the following models of the VASIMR helicon discharge have been further d...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
The following paper outlines the importance of vacuum ultraviolet (VUV) aerothermodynamic heating du...
Abstract: We have significantly upgraded the capability of the Variable Specific Impulse Magnetoplas...
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is a high power magnetoplasma rocket, ca...
Plasma processes can present dicult control challenges due to time-varying dynamics and a lack of r...