A Theoretical Study of the Motion of an Idealized Plasma Ring Under the Influence of Various Coaxial Magnetic Fields

A Theoretical Study of the Motion of an Idealized Plasma Ring Under the Influence of Various Coaxial Magnetic Fields PDF Author: Clarence W. Matthews
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ISBN:
Category : Particle accelerators
Languages : en
Pages : 48

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 246

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NASA Technical Note

NASA Technical Note PDF Author:
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ISBN:
Category :
Languages : en
Pages : 346

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Nuclear Science Abstracts

Nuclear Science Abstracts PDF Author:
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ISBN:
Category : Nuclear energy
Languages : en
Pages : 1028

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ARL [report]

ARL [report] PDF Author:
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Category :
Languages : en
Pages : 884

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Controlled Fusion and Plasma Research

Controlled Fusion and Plasma Research PDF Author:
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Category : Controlled fusion
Languages : en
Pages : 578

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TID.

TID. PDF Author:
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Category : Energy development
Languages : en
Pages : 212

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Nuclear Science Abstracts

Nuclear Science Abstracts PDF Author:
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ISBN:
Category : Nuclear energy
Languages : en
Pages : 1036

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Plasma Physics and Magnetohydrodynamics

Plasma Physics and Magnetohydrodynamics PDF Author: Defense Documentation Center (U.S.)
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Category : Magnetohydrodynamics
Languages : en
Pages : 290

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Characteristics of a Continuous-flow Induction Plasma Accelerator

Characteristics of a Continuous-flow Induction Plasma Accelerator PDF Author: J. D. Brooks
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Category : Plasma accelerators
Languages : en
Pages : 36

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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.