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Mass, momentum and energy flow from an MPD acceleratorThe mass, momentum, and energy flows are measured over a current range of 8 to 50 kA and inlet mass flows of 2 to 36q/sec of argon. The momentum flux profile indicates that the accelerator produces a uniform, 2-inch diameter axial jet at the anode which expands into a Gaussian profile at an axial station 11 inches from the anode. The electromagnetic component of the thrust is found to follow the familiar quadratic dependence on arc current, while a more complex empirical relation is needed to correlate the gasdynamic contribution with the current and mass flow rate. Using available time-of-flight velocity profiles at a current of 16 kA and a mass flow of 5.9 g/sec, calculated flux profiles of mass and kinetic energy exhibit a tendency for some fraction of the inlet mass flow to leak out at a low velocity around the central high velocity core.
Document ID
19720019032
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Cory, J. S.
(Princeton Univ. NJ, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-127120
REPT-999
Report Number: NASA-CR-127120
Report Number: REPT-999
Accession Number
72N26682
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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