Author: Clarence W. Matthews
Publisher:
ISBN:
Category : Particle accelerators
Languages : en
Pages : 48
Book Description
A Theoretical Study of the Motion of an Idealized Plasma Ring Under the Influence of Various Coaxial Magnetic Fields
Author: Clarence W. Matthews
Publisher:
ISBN:
Category : Particle accelerators
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Particle accelerators
Languages : en
Pages : 48
Book Description
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 246
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 246
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 346
Book Description
Nuclear Science Abstracts
Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1028
Book Description
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1028
Book Description
ARL [report]
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 884
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 884
Book Description
Controlled Fusion and Plasma Research
Author:
Publisher:
ISBN:
Category : Controlled fusion
Languages : en
Pages : 578
Book Description
Publisher:
ISBN:
Category : Controlled fusion
Languages : en
Pages : 578
Book Description
TID.
Author:
Publisher:
ISBN:
Category : Energy development
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category : Energy development
Languages : en
Pages : 212
Book Description
Nuclear Science Abstracts
Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1036
Book Description
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1036
Book Description
Plasma Physics and Magnetohydrodynamics
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Magnetohydrodynamics
Languages : en
Pages : 290
Book Description
Publisher:
ISBN:
Category : Magnetohydrodynamics
Languages : en
Pages : 290
Book Description
Characteristics of a Continuous-flow Induction Plasma Accelerator
Author: J. D. Brooks
Publisher:
ISBN:
Category : Plasma accelerators
Languages : en
Pages : 36
Book Description
Characteristics of continuous-flow induction plasma accelerators with a 10-kilocycle, single-phase driving coil on supersonic nozzles were studied. Pressure measurements and vane-deflection measurements were made in a 15-centimeter-diameter accelerator at various mass flow rates. Charged-particle velocities were obtained in 15-centimeter-diameter and 10-centimeter-diameter accelerators by measuring with photoelectric detectors the time required for a change in flow luminosity to travel a known distance. Pressure-probe measurements indicated that the entire flow, including the boundary layer and the separated-flow region, was accelerated in the 15-centimeter-diameter accelerator. The largest increase in pilot pressure was 250 percent of the cold-flow value with 20 kilowatts of 10-kilocycle driving power. The charged-particle velocities increased as the mass flow rate was reduced and as the power was increased. The maximum charged-particle velocity obtained was 40,000 meters per second in the 10-centimeter-diameter accelerator. Average velocity and thrust obtained from vane-deflection measurements were in good agreement with those obtained from pressure-probe measurements.
Publisher:
ISBN:
Category : Plasma accelerators
Languages : en
Pages : 36
Book Description
Characteristics of continuous-flow induction plasma accelerators with a 10-kilocycle, single-phase driving coil on supersonic nozzles were studied. Pressure measurements and vane-deflection measurements were made in a 15-centimeter-diameter accelerator at various mass flow rates. Charged-particle velocities were obtained in 15-centimeter-diameter and 10-centimeter-diameter accelerators by measuring with photoelectric detectors the time required for a change in flow luminosity to travel a known distance. Pressure-probe measurements indicated that the entire flow, including the boundary layer and the separated-flow region, was accelerated in the 15-centimeter-diameter accelerator. The largest increase in pilot pressure was 250 percent of the cold-flow value with 20 kilowatts of 10-kilocycle driving power. The charged-particle velocities increased as the mass flow rate was reduced and as the power was increased. The maximum charged-particle velocity obtained was 40,000 meters per second in the 10-centimeter-diameter accelerator. Average velocity and thrust obtained from vane-deflection measurements were in good agreement with those obtained from pressure-probe measurements.