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Kaufman thruster development at Lewis Research Center (LeRC)The current status of research programs on mercury electron bombardment thrusters is reviewed. Future thruster requirements predicted from mission analysis are briefly discussed to establish the relationship with present programs. Thrusters ranging in size from 5 to 150 cm diameter are described. These thrusters have possible near to far term applications extending from stationkeeping to primary propulsion. Beam currents range from 10 mA at to 25 A at accelerating potentials of 500 to 5000 V.
Document ID
19720018955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kerslake, W. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Reader, P. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Publication Information
Publication: BNL Proc. of the Symp. on Ion Sources and Formation of Ion Beams
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-68385
Accession Number
72N26605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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