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Effect of cathode configuration on 30 kWe arcjet electrical characteristicsThis paper compares the electrical characteristics of a 30 kWe arcjet for four cathode tip geometries. The electrical behavior of various cathode configurations is characterized by examining engine operation over a range of power levels (20 kWe - 30 kWe), current levels (200 A - 300 A) and geometric arc lengths (0.85 cm - 1.81 cm). Preliminary results indicate that tip geometry does not affect arc current or engine power when plotted as a function of geometric arc length, that at a fixed power the current level can be expected to drop as the arc grows in length due to erosion, and that any long duration test will require adjustment of the power source to maintain a constant power level.
Document ID
19890059335
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chopra, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Deininger, W. D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
King, D. Q.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 89-2261
Accession Number
89A46706
Distribution Limits
Public
Copyright
Other

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