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Microwave Driven Magnetic Plasma Accelerator Studies (CYCLOPS) A microwave-driven cyclotron resonance plasma acceleration device was investigated using argon, krypton, xenon, and mercury as propellants. Limited ranges of propellant flow rate, input power, and magnetic field strength were used. Over-all efficiencies (including the 65% efficiency of the input polarizer) less than 10% were obtained for specific impulse values between 500 and 1500 sec. Power transfer efficiencies, however, approached 100% of the input power available in the right-hand component of the incident circularly polarized radiation. Beam diagnostics using Langmuir probes, cold gas mapping, r-f mapping and ion energy analyses were performed in conjunction with an engine operating in a pulsed mode. Measurements of transverse electron energies at the position of cyclotron resonant absorption yielded energy values more than an order of magnitude lower than anticipated. The measured electron energies were, however, consistent with the low values of average ion energy measured by retarding potential techniques. The low values of average ion energy were also consistent with the measured thrust values. It is hypothesized that ionization and radiation limit the electron kinetic energy to low-values thus limiting the energy which is finally transferred to the ion. Thermalization by electron-electron collision was also identified as an additional loss mechanism. The use of light alkali metals, which have relatively few low lying energy levels to excite, with the input power to mass ratio selected so as to limit the electron energies to less than the second ionization potential, is suggested. It is concluded, however, that the over-all efficiency for such propellants would be less than 40 per cent.
Document ID
19670018272
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Crimi, G. F.
(General Electric Co. Philadelphia, PA, United States)
Eckert, A. C.
(General Electric Co. Philadelphia, PA, United States)
Miller, D. B.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 3, 2013
Publication Date
March 24, 1967
Subject Category
Plasma Physics
Report/Patent Number
NASA-CR-72227
GRC-E-DAA-TN51047
Accession Number
67N27601
Funding Number(s)
CONTRACT_GRANT: NAS3-8903
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
CYCLOPS PLASMA ACCELERATOR
SPACECRAFT PROPULSION
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