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SERT 2 hollow cathode multiple restarts in spaceFuture missions, both station keeping and primary electric propulsion, will require multiple thrust restarts after periods of inactivity from a few hours to over one year. Although not a part of the original SERT 2 (Space Electric Rocket Test) flight objective, the opportunity to demonstrate multiple cathode restarts in space became available following completion of thruster running. Both neutralizer and main cathodes of each flight thruster were restarted repeatedly following storage periods up to 490 days. No deterioration of cathode heaters was noted nor was any change required in starting voltages or currents.
Document ID
19730022010
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kerslake, W. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Finke, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
E-7638
NASA-TM-X-68292
Report Number: E-7638
Report Number: NASA-TM-X-68292
Meeting Information
Meeting: Elec. Propulsion Conf.
Location: Lake Tahoe, NV
Country: United States
Start Date: October 31, 1973
End Date: November 2, 1973
Sponsors: AIAA
Accession Number
73N30742
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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