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Arc-Jet Thrustor DevelopmentTwo flight-type 1.4-kW hydrazine arcjet systems developed and tested under Lewis program. Each consists of thrustor, gas generator, and power-processing unit. Performance significantly improved. Technology transferred to user community, and first commercial flight anticipated in 1993.
Document ID
19930000236
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Curran, F. M. (NASA Lewis Research Center, Cleveland, OH.)
Hamley, J. A. (NASA Lewis Research Center, Cleveland, OH.)
Gruber, R. P. (NASA Lewis Research Center, Cleveland, OH.)
Sankovic, J. M. (NASA Lewis Research Center, Cleveland, OH.)
Haag, T. W. (NASA Lewis Research Center, Cleveland, OH.)
Marren, W. E. (NASA Lewis Research Center, Cleveland, OH.)
Sarmiento, C. J. (NASA Lewis Research Center, Cleveland, OH.)
Carney, L. (NASA Lewis Research Center, Cleveland, OH.)
Date Acquired
August 16, 2013
Publication Date
April 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-15284
Accession Number
93B10236
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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