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Arcjet thruster research and technologyThe design, analysis, and performance testing of an advanced lower power arcjet is described. A high impedance, vortex stabilized 1-kw class arcjet has been studied. A baseline research thruster has been built and endurance and performance tested. This advanced arcjet has demonstrated long lifetime characteristics, but lower than expected performance. Analysis of the specific design has identified modifications which should improve performance and maintain the long life time shown by the arcjet.
Document ID
19880008348
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Makel, Darby B.
(Aerojet TechSystems Co. Sacramento, CA., United States)
Cann, Gordon L.
(Technion, Inc. Irvine, Calif., United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-180865
NAS 1.26:180865
RPT/BB0642
Report Number: NASA-CR-180865
Report Number: NAS 1.26:180865
Report Number: RPT/BB0642
Accession Number
88N17732
Funding Number(s)
CONTRACT_GRANT: NAS3-24842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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