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Acceleration processes in the quasi-steady magnetoplasmadynamic dischargeThe flow field characteristics within the discharge chamber and exhaust of a quasi-steady magnetoplasmadynamic (MPD) arcjet were examined to clarify the nature of the plasma acceleration process. The observation of discharge characteristics unperturbed by insulator ablation and terminal voltage fluctuations, first requires the satisfaction of three criteria: the use of refractory insulator materials; a mass injection geometry tailored to provide propellant to both electrode regions of the discharge; and a cathode of sufficient surface area to permit nominal MPD arcjet operation for given combinations of arc current and total mass flow. The axial velocity profile and electromagnetic discharge structure were measured for an arcjet configuration which functions nominally at 15.3 kA and 6 g/sec argon mass flow. An empirical two-flow plasma acceleration model is advanced which delineates inner and outer flow regions and accounts for the observed velocity profile and calculated thrust of the accelerator.
Document ID
19750005557
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Boyle, M. J.
(Princeton Univ. NJ, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1974
Subject Category
Plasma Physics
Report/Patent Number
NASA-CR-141103
REPT-1188
Accession Number
75N13629
Funding Number(s)
CONTRACT_GRANT: NGL-31-001-005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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