NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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.
No Preview Available