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Development and initial operating characteristics of the 20 megawatt linear plasma accelerator facilityA 20-megawatt linear plasma accelerator facility, a steady flow, Faraday-type plasma accelerator facility for high velocity aerodynamic testing, was constructed, developed, and brought to an operational status. The accelerator has a 63.5-mm-square and 0.5-meter-long channel and utilizes nitrogen-seeded with 2 % mole fraction of cesium vapor. Modification of the original accelerator design characteristics and the improvements necessary to make the arc heater a suitable plasma source are described. The measured accelerator electrode current distribution and the electrode-wall potential distributions are given. The computed and the measured values are in good agreement. Measured pitot pressure indicates that an accelerator exit velocity of 9.2 km/sec, is obtained with 30 of the 36 electrode pairs powered and corresponds to a velocity increase to about 2 1/4 times the computed entrance velocity. The computed stagnation enthalpy at the accelerator exit is 92 MJ/kg, and the mass density corresponds to an altitude of about 58 km. The 92 MJ/kg stagnation enthalpy corresponds to a kinetic energy content at low temperature equivalent to a velocity of 13.6 km/sec.
Document ID
19720005094
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Carter, A. F.
(NASA Langley Research Center Hampton, VA, United States)
Weaver, W. R.
(NASA Langley Research Center Hampton, VA, United States)
Mcfarland, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Wood, G. P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Physics, Plasma
Report/Patent Number
L-7932
NASA-TN-D-6547
Report Number: L-7932
Report Number: NASA-TN-D-6547
Accession Number
72N12743
Funding Number(s)
PROJECT: RTOP 112-02-22-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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