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Propagation of charge-exchange plasma produced by an ion thrusterUnder the proper conditions there is an end-effect of a long, cylindrical Langmuir probe which allows a significant increase in collected ion current when the probe is aligned with a flowing plasma. This effect was used to determine the charge-exchange plasma flow direction at various locations relative to the ion thruster. The ion current collected by the probe as a function of its angle with respect to the plasma flow allows determination of the plasma density and plasma flow velocity at the probe's location upstream of the ion thruster optics. The density values obtained from the ion current agreed to within a factor of two of density values obtained by typical voltage-current Langmuir probe characteristics.
Document ID
19810008612
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Carruth, M. R., Jr.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Brady, M. E.
(Boeing Aerospace Co. Pasadena, Calif., United States)
Date Acquired
August 11, 2013
Publication Date
January 15, 1981
Publication Information
Publication: Exptl. and Anal. Evaluation of Ion Thruster(Spacecraft Interactions
Subject Category
Spacecraft Propulsion And Power
Accession Number
81N17132
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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