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Durability tests of a five centimeter diameter ion thruster systemA modified Hughes SIT-5 system is being tested for durability at the Lewis Research Center. As of October 1, 1972, the thruster subsystem has logged over 8000 hours of operation. The initial 2023 hours were run with a translating screen thrust vector grid. The thruster is currently operating with an electrostatic type vector grid. Profiles and maps taken at widely separated intervals show that performance and operating characteristics have remained essentially constant. Overall efficiency is about 32 percent and power to thrust ratio is 170 watts per millipound at a specific impulse of 2500 seconds. Telescopic examination of the vector grid shows some sputtering erosion due to charge exchange and direct impingement ions.
Document ID
19720026099
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nakanishi, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
E-7128
NASA-TM-X-68132
Report Number: E-7128
Report Number: NASA-TM-X-68132
Meeting Information
Meeting: Propulsion Joint Specialists Conf.
Location: New Orleans
Start Date: November 29, 1972
End Date: December 1, 1972
Sponsors: Soc. of Automotive Engr., AIAA
Accession Number
72N33749
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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