NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Advanced electric propulsion and space plasma contactor researchA theory of the plasma contacting process is described and experimental results obtained using three different hollow cathode-based plasma contactors are presented. The existence of a sheath across which the bulk of the voltage drop associated with the contacting process occurs is demonstrated. Test results are shown to agree with a model of a spherical, space-charge-limited double sheath. The concept of ignited mode contactor operation is discussed, which is shown to enhance contactor efficiency when it is collecting electrons. An investigation of the potentials in the plasma plumes downstream of contactors operating at typical conditions is presented. Results of tests performed on hollow cathodes operating at high interelectrode pressures (up to about 1000 Torr) on ammonia are presented and criteria that are necessary to ensure that the cathode will operate properly in this regime are presented. These results suggest that high pressure hollow cathode operation is difficult to achieve and that special care must be taken to assure that the electron emission region remains diffuse and attached to the low work function insert. Experiments conducted to verify results obtained previously using a ring cusp ion source equipped with a moveable anode are described and test results are reported. A theoretical study of hollow cathode operation at high electron emission currents is presented. Preliminary experiments using the constrained sheath optics concept to achieve ion extraction under conditions of high beam current density, low net accelerating voltage and well columniated beamlet formation are discussed.
Document ID
19880004744
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilbur, Paul J.
(Colorado State Univ. Fort Collins, CO, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:180862
NASA-CR-180862
Report Number: NAS 1.26:180862
Report Number: NASA-CR-180862
Accession Number
88N14126
Funding Number(s)
CONTRACT_GRANT: NGR-06-002-112
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available